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OPS 0100 (TRANSIT 15), 2754

Orbit data source: Space-Track

OPS 0100 (TRANSIT 15), 2754 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Fri, 14 Apr 1967 UTC via an SCOUT A launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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https://www.satcat.com/sats-embedded/2754?theme=dark&initialShowStats=false

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Identifier

2754, 1967-034A

Orbit

LEO

Country

Related business

United States Navy (US)

Manufacturer

APL

Mission

Spacecraft

Bus & Motor

TRANSIT 5, Unknown motor

Mass

~50 kg wet, ~50 kg dry

Launch date (UTC)

1967-04-14 (60 years ago)

Launch vehicle

SCOUT A

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

OCT CYL + 4 PAN + ANT, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 OPS 0100 (TRANSIT 15)
1 02754U 67034A   26304.72684522  .00000101  00000-0  12862-3 0  9993
2 02754  90.2458  38.4751 0021553 106.3231  46.4785 13.57429345944631

Epoch: 2026-10-31T17:26Z

TLE epoch observation values (Epoch: 2026-10-31T17:26:39.427Z)

Latitude

27.05412°

Longitude

-83.09272°

Altitude

1,037.416 km

Speed

7.341 km/s

True Right ascension

14h 34m 23s

True Declination

26° 55' 13"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

02:49:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,058.081 km

Perigee altitude

1,026.095 km

Semi-major axis

7,420.225 km

Eccentricity

0.00216

Inclination

90.2458°

RAAN

38.4751°

Arg. of periapsis

106.3231°

True anomaly

46.65792°

Mean anomaly

46.4785°

Eccentric anomaly

46.56818°

Mean motion

3.39561 °/min

Orbital period

106.02 mins

BSTAR

0.00012862

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Other satellites on launch #34 in the year 1967 (1967-04-14 UTC)

TRANSIT 15 DEB, 29180 (Decayed)

TRANSIT 15 DEB, 7670 (Decayed)

TRANSIT 15 DEB, 29265 (Decayed)

TRANSIT 15 DEB, 29276 (Decayed)

SCOUT A DEB, 2777

SCOUT A DEB, 6718 (Decayed)

TRANSIT 15 DEB, 22172 (Decayed)

OPS 0100 DEB *, 4843

SCOUT A R/B, 2755

SCOUT A DEB, 2778

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OPS 0100 (TRANSIT 15) Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
10 mins	2026-11-01 18:04:07.119Z	21.575° NNE	2026-11-01 18:09:07.119Z	90.996° ESE	42.633°	2026-11-01 18:14:07.119Z	153.513° SSE
8 mins	2026-11-01 19:51:07.119Z	328° NNW	2026-11-01 19:54:07.119Z	290.676° WNW	28.899°	2026-11-01 19:59:07.119Z	231.374° WSW
10 mins	2026-11-02 05:58:07.119Z	141.117° SSE	2026-11-02 06:03:07.119Z	72.085° E	40.664°	2026-11-02 06:08:07.119Z	14.567° NNE

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out OPS 0100 (TRANSIT 15), 2754 on other resources

View OPS 0100 (TRANSIT 15), 2754 on NASA - NSSDCA Website

View OPS 0100 (TRANSIT 15), 2754 on Heavens-Above

View OPS 0100 (TRANSIT 15), 2754 on Keep Track

View OPS 0100 (TRANSIT 15), 2754 on Celestrak

View OPS 0100 (TRANSIT 15), 2754 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

OPS 0100 (TRANSIT 15), 2754

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-10-31T17:26:39.427Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #34 in the year 1967 (1967-04-14 UTC)

OPS 0100 (TRANSIT 15) Visibility forecast

Co-orbital & Co-planar RSOs

Check out OPS 0100 (TRANSIT 15), 2754 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago