OPS 9312 (IDSCS 2), 2216
Orbit data source: Space-Track
OPS 9312 (IDSCS 2), 2216 is a payload satellite owned by USAF SSD (US) in GEO that was launched on Thu, 16 Jun 1966 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). 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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2216 intel report (Beta)
OPS 9312 (IDSCS 2) details
Identifier | |
Orbit | GEO |
Last TLE update | 1 day ago |
Origin | |
Manufacturer | Philco-Ford WDL |
Mission | Non-operational Defense Communications |
Bus & Motor | IDCSP, Unknown motor |
Mass | 45 kg wet, 45 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Ico Poly, 0.9 m |
Radar Cross Section | 0.926 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 OPS 9312 (IDSCS 2)
1 02216U 66053C 24355.35095896 -.00000066 00000-0 00000-0 0 9998
2 02216 7.6460 48.7316 0033688 204.1385 154.7687 1.07850551 43395
Epoch: 2024-12-20T08:25Z
Definitive object data (Epoch: 2024-12-20T08:25:22.854Z)
Latitude | -0.11584° |
Longitude | -167.9466° |
Altitude | 33,909.648 km |
Speed | 3.141 km/s |
True Right ascension | 03h 11m 15s |
True Declination | 0° 06' 57" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 7.52867° |
Longitude | -66.05316° |
Altitude | 33,817.132 km |
Speed | 3.148 km/s |
Apparent Right ascension | 09h 42m 44s |
Apparent Declination | 1° 54' 28" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 12:01:59 |
Azimuth | 228.715° WSW |
Elevation | 40.596° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 33,923.807 km |
Perigee altitude | 33,653.18 km |
Semi-major axis | 40,166.631 km |
Eccentricity | 0.0033688 |
Inclination | 7.646° |
RAAN | 48.7316° |
Arg. of periapsis | 204.1385° |
True anomaly | 154.93263° |
Mean anomaly | 154.7687° |
Eccentric anomaly | 154.85073° |
Mean motion | 0.26962 °/min |
BSTAR | Unknown |
Orbital period | 1335.23 mins |
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2216 neighbors
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Other satellites on launch #53 in the year 1966 (1966-06-16 UTC)
OPS 9312 (IDSCS 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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1440 mins | 2024-12-21 13:00:05.932Z | 228.698° WSW | 2024-12-22 10:53:05.932Z | 190.959° SSW | 38.104° | 2024-12-22 13:00:05.932Z | 185.935° SSW |
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