OPS 9323 (IDSCS 10), 2650
Orbit data source: Space-Track
OPS 9323 (IDSCS 10), 2650 is a payload satellite owned by USAF SSD (US) in GEO that was launched on Wed, 18 Jan 1967 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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2650 intel report (Beta)
OPS 9323 (IDSCS 10) details
Identifier | |
Orbit | GEO |
Last TLE update | 2 days 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 2 days ago
0 OPS 9323 (IDSCS 10)
1 02650U 67003C 25039.01753672 -.00000121 00000-0 00000-0 0 9994
2 02650 7.3639 49.1227 0033107 98.0712 237.6208 1.08222384135095
Epoch: 2025-02-08T00:25Z
Definitive object data (Epoch: 2025-02-08T00:25:15.172Z)
Latitude | -3.07855° |
Longitude | -119.98855° |
Altitude | 33,766.625 km |
Speed | 3.148 km/s |
True Right ascension | 01h 38m 47s |
True Declination | -3° 04' 31" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -6.8337° |
Longitude | 152.17384° |
Altitude | 33,811.259 km |
Speed | 3.145 km/s |
Apparent Right ascension | 20h 03m 55s |
Apparent Declination | -13° 52' 15" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 17:40:29 |
Azimuth | 140.455° SSE |
Elevation | 26.722° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 33,829.119 km |
Perigee altitude | 33,563.769 km |
Semi-major axis | 40,074.581 km |
Eccentricity | 0.0033107 |
Inclination | 7.3639° |
RAAN | 49.1227° |
Arg. of periapsis | 98.0712° |
True anomaly | 237.30112° |
Mean anomaly | 237.6208° |
Eccentric anomaly | 237.46089° |
Mean motion | 0.27055 °/min |
BSTAR | Unknown |
Orbital period | 1330.65 mins |
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2650 neighbors
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Other satellites on launch #3 in the year 1967 (1967-01-18 UTC)
OPS 9323 (IDSCS 10) 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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1323 mins | 2025-02-09 15:21:05.459Z | 140.466° SSE | 2025-02-10 01:42:05.459Z | 119.07° SE | 26.873° | 2025-02-10 13:24:05.459Z | 116.873° SE |
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