OPS 4682 DEB, 1399

Orbit data source: Space-Track

OPS 4682 DEB, 1399 is space debris in LEO originally from a launch on Sat, 03 Apr 1965 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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<iframe src="https://www.satcat.com/sats-embedded/1399?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/1399?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1399, 1965-027E

Orbit

LEO

Last TLE update

6 days ago

Origin

United States Air Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1965-04-03 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 6 days ago

0 OPS 4682 DEB
1 01399U 65027E   25177.25005321  .00000412  00000-0  13496-2 0  9994
2 01399  90.2576  16.3698 0010397 137.6233 222.5694 12.99740699586860

Epoch: 2025-06-26T06:00Z

TLE epoch observation values (Epoch: 2025-06-26T06:00:04.597Z)

Latitude

0.00001°

Longitude

11.73068°

Altitude

1,271.842 km

Speed

7.217 km/s

True Right ascension

01h 05m 28s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

23.49°

Longitude

-168.01991°

Altitude

1,259.354 km

Speed

7.231 km/s

Apparent Right ascension

13h 14m 14s

Apparent Declination

-26° 16' 51"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

13:03:07

Azimuth

177.28° S

Elevation

23.753°

Doppler factor

Orbital elements

Apogee altitude

1,268.172 km

Perigee altitude

1,252.289 km

Semi-major axis

7,638.367 km

Eccentricity

0.00104

Inclination

90.2576°

RAAN

16.3698°

Arg. of periapsis

137.6233°

True anomaly

Unknown

Mean anomaly

222.5694°

Eccentric anomaly

Unknown

Mean motion

3.25119 °/min

Orbital period

110.73 mins

BSTAR

0.0013496

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Other satellites on launch #27 in the year 1965 (1965-04-03 UTC)

OPS 4682 (SNAPSHOT), 1314

OPS 4682 DEB Visibility forecast

Observer location: undefined°, undefined°

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.
8 mins	2025-07-02 03:03:13.865Z	322.373° NNW	2025-07-02 03:07:13.865Z	286.067° WNW	17.48°	2025-07-02 03:11:13.865Z	252.486° W
9 mins	2025-07-02 11:48:13.865Z	111.425° ESE	2025-07-02 11:52:13.865Z	74.702° E	20.798°	2025-07-02 11:57:13.865Z	28.836° NE
13 mins	2025-07-02 13:36:13.865Z	189.218° SSW	2025-07-02 13:42:13.865Z	265.557° W	42.753°	2025-07-02 13:49:13.865Z	351.547° N
6 mins	2025-07-02 23:24:13.865Z	53.524° ENE	2025-07-02 23:26:13.865Z	70.286° E	13.527°	2025-07-02 23:30:13.865Z	103.203° ESE
10 mins	2025-07-03 01:12:13.865Z	4.063° NNE	2025-07-03 01:18:13.865Z	79.867° E	44.906°	2025-07-03 01:22:13.865Z	180.425° SSW

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Check out OPS 4682 DEB, 1399 on other resources

View OPS 4682 DEB, 1399 on Heavens-Above

View OPS 4682 DEB, 1399 on Keep Track

View OPS 4682 DEB, 1399 on Celestrak

View OPS 4682 DEB, 1399 on Gunter's Space Page

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