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DODECAPOLE 2, 1510

Orbit data source: Space-Track

DODECAPOLE 2, 1510 is a payload satellite owned by NRL (US) in LEO that was launched on Fri, 13 Aug 1965 UTC via a THOR ABLESTAR 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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<iframe src="https://www.satcat.com/sats-embedded/1510?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/1510?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1510, 1965-065C

Orbit

LEO

Last TLE update

11 hours ago

Origin

United States Navy (US)

Manufacturer

NRL

Mission

Defense Calibration

Bus & Motor

NRL 9", Unknown motor

Mass

4 kg wet, 4 kg dry

Launch date (UTC)

1965-08-13 (60 years ago)

Launch vehicle

THOR ABLESTAR

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Sphere + 12 Rod, 15.2 m

Radar Cross Section

0.071 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 11 hours ago

0 DODECAPOLE 2
1 01510U 65065C   25183.83902114  .00002852  00000-0  16556-2 0  9998
2 01510  90.0566  22.6081 0034986 216.7669 143.1114 14.08239170983955

Epoch: 2025-07-02T20:08Z

TLE epoch observation values (Epoch: 2025-07-02T20:08:11.426Z)

Latitude

-0.00011°

Longitude

159.44612°

Altitude

888.746 km

Speed

7.397 km/s

True Right ascension

01h 30m 25s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-52.59357°

Longitude

-20.62453°

Altitude

861.678 km

Speed

7.433 km/s

Apparent Right ascension

10h 09m 04s

Apparent Declination

-57° 02' 19"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

19:13:59

Azimuth

223.876° SW

Elevation

-57.112°

Doppler factor

Orbital elements

Apogee altitude

887.7 km

Perigee altitude

837.037 km

Semi-major axis

7,240.506 km

Eccentricity

0.0035

Inclination

90.0566°

RAAN

22.6081°

Arg. of periapsis

216.7669°

True anomaly

Unknown

Mean anomaly

143.1114°

Eccentric anomaly

Unknown

Mean motion

3.52281 °/min

Orbital period

102.19 mins

BSTAR

0.0016556

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Other satellites on launch #65 in the year 1965 (1965-08-13 UTC)

THOR ABLESTAR DEB, 1504

THOR ABLESTAR R/B, 1508

THOR ABLESTAR DEB, 1511

TEMPSAT 1, 1512

OPS 8464 (TRANSIT 5B-7), 1514

NAVSPASUR ROD 1, 1515

CALSPHERE 4(A), 1520

PORCUPINE 2, 1577

THOR ABLESTAR DEB, 1521

THOR ABLESTAR DEB, 1522

OPS 8464 DEB *, 2335 (Decayed)

TRANSIT 5B-7 DEB, 3809 (Decayed)

THOR ABLESTAR DEB, 3810

THOR ABLESTAR DEB, 5265

DODECAPOLE 2 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.
10 mins	2025-07-03 13:18:08.926Z	159.788° S	2025-07-03 13:23:08.926Z	69.739° E	40.735°	2025-07-03 13:28:08.926Z	6.054° NNE
5 mins	2025-07-03 15:03:08.926Z	253.245° W	2025-07-03 15:05:08.926Z	277.281° WNW	16.793°	2025-07-03 15:08:08.926Z	312.735° NW
9 mins	2025-07-04 01:43:08.926Z	359.368° N	2025-07-04 01:47:08.926Z	326.722° NNW	43.997°	2025-07-04 01:52:08.926Z	188.561° SSW

Authenticating...

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Check out DODECAPOLE 2, 1510 on other resources

View DODECAPOLE 2, 1510 on NASA - NSSDCA Website

View DODECAPOLE 2, 1510 on Heavens-Above

View DODECAPOLE 2, 1510 on Keep Track

View DODECAPOLE 2, 1510 on Celestrak

View DODECAPOLE 2, 1510 on Gunter's Space Page

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