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). Payloads include a variety of satellites, spacecraft, and rockets 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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Edit Public Description
Identifier | |
Orbit | LEO |
Last TLE update | 17 hours ago |
Origin | |
Manufacturer | NRL |
Mission | Defense Calibration |
Bus & Motor | NRL 9", Unknown motor |
Mass | 4 kg wet, 4 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
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 17 hours ago
0 DODECAPOLE 2
1 01510U 65065C 25077.36823671 .00010682 00000-0 63414-2 0 9993
2 01510 90.0561 21.9508 0034217 193.1867 166.8425 14.07127149968974
Epoch: 2025-03-18T08:50Z
Definitive object data (Epoch: 2025-03-18T08:50:15.651Z)
Latitude | -0.00006° |
Longitude | 73.21387° |
Altitude | 896.412 km |
Speed | 7.391 km/s |
True Right ascension | 01h 27m 48s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 67.06154° |
Longitude | 73.08652° |
Altitude | 894.642 km |
Speed | 7.404 km/s |
Apparent Right ascension | 21h 07m 19s |
Apparent Declination | 25° 52' 38" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 07:00:28 |
Azimuth | 330.2° NNW |
Elevation | -17.878° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 890.974 km |
Perigee altitude | 841.398 km |
Semi-major axis | 7,244.323 km |
Eccentricity | 0.0034217 |
Inclination | 90.0561° |
RAAN | 21.9508° |
Arg. of periapsis | 193.1867° |
True anomaly | 166.93138° |
Mean anomaly | 166.8425° |
Eccentric anomaly | 166.88698° |
Mean motion | 3.52003 °/min |
BSTAR | 0.0063414 |
Orbital period | 102.27 mins |
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Other satellites on launch #65 in the year 1965 (1965-08-13 UTC)
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. |
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8 mins | 2025-03-19 07:37:23.858Z | 31.765° NE | 2025-03-19 07:41:23.858Z | 85.585° E | 24.35° | 2025-03-19 07:45:23.858Z | 137.138° SSE |
8 mins | 2025-03-19 09:20:23.858Z | 332.976° NNW | 2025-03-19 09:23:23.858Z | 282.776° WNW | 30.677° | 2025-03-19 09:28:23.858Z | 215.837° SW |
5 mins | 2025-03-19 19:08:23.858Z | 96.865° ESE | 2025-03-19 19:10:23.858Z | 73.862° E | 15.248° | 2025-03-19 19:13:23.858Z | 40.6° NE |
10 mins | 2025-03-19 20:47:23.858Z | 187.954° SSW | 2025-03-19 20:52:23.858Z | 294.331° NW | 42.436° | 2025-03-19 20:57:23.858Z | 351.945° N |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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