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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1510 intel report (Beta)
DODECAPOLE 2 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 20 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 20 hours ago
0 DODECAPOLE 2
1 01510U 65065C 24355.78747683 .00005253 00000-0 31911-2 0 9990
2 01510 90.0519 21.4457 0038255 115.2158 245.2998 14.05768690956669Epoch: 2024-12-20T18:53Z
Definitive object data (Epoch: 2024-12-20T18:53:57.998Z)
| Latitude | 0° |
| Longitude | 8.10607° |
| Altitude | 888.605 km |
| Speed | 7.402 km/s |
| True Right ascension | 01h 25m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -26.19292° |
| Longitude | -171.91459° |
| Altitude | 885.25 km |
| Speed | 7.408 km/s |
| Apparent Right ascension | 12h 37m 39s |
| Apparent Declination | -77° 02' 02" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:41:59 |
| Azimuth | 184.014° SSW |
| Elevation | -27.384° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 898.587 km |
| Perigee altitude | 843.125 km |
| Semi-major axis | 7,248.993 km |
| Eccentricity | 0.0038255 |
| Inclination | 90.0519° |
| RAAN | 21.4457° |
| Arg. of periapsis | 115.2158° |
| True anomaly | 244.90234° |
| Mean anomaly | 245.2998° |
| Eccentric anomaly | 245.10099° |
| Mean motion | 3.51663 °/min |
| BSTAR | 0.0031911 |
| Orbital period | 102.37 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2024-12-22 01:46:49.365Z | 146.707° SSE | 2024-12-22 01:50:49.365Z | 69.444° E | 36.104° | 2024-12-22 01:54:49.365Z | 13.17° NNE |
| 7 mins | 2024-12-22 03:29:49.365Z | 238.623° WSW | 2024-12-22 03:32:49.365Z | 276.367° WNW | 19.798° | 2024-12-22 03:36:49.365Z | 324.542° NNW |
| 9 mins | 2024-12-22 14:11:49.365Z | 4.51° NNE | 2024-12-22 14:15:49.365Z | 37.617° NE | 44.49° | 2024-12-22 14:20:49.365Z | 180.774° SSW |
Authenticating...
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