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 | 11 hours 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 11 hours ago
0 OPS 9323 (IDSCS 10)
1 2650U 67003C 24356.08285972 -.00000105 00000-0 00000+0 0 9996
2 2650 7.2719 49.5218 0033810 98.1535 251.7850 1.08222236134569
Epoch: 2024-12-21T01:59Z
Definitive object data (Epoch: 2024-12-21T01:59:19.079Z)
Latitude | -1.30884° |
Longitude | -80.79036° |
Altitude | 33,737.246 km |
Speed | 3.151 km/s |
True Right ascension | 02h 36m 42s |
True Declination | -1° 18' 27" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 1.37619° |
Longitude | 98.67118° |
Altitude | 33,650.466 km |
Speed | 3.157 km/s |
Apparent Right ascension | 14h 53m 42s |
Apparent Declination | -4° 53' 54" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 12:01:45 |
Azimuth | 128.125° SE |
Elevation | 30.279° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 33,831.974 km |
Perigee altitude | 33,560.989 km |
Semi-major axis | 40,074.619 km |
Eccentricity | 0.003381 |
Inclination | 7.2719° |
RAAN | 49.5218° |
Arg. of periapsis | 98.1535° |
True anomaly | 251.41747° |
Mean anomaly | 251.785° |
Eccentric anomaly | 251.60119° |
Mean motion | 0.27054 °/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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1356 mins | 2024-12-21 12:59:52.097Z | 128.14° SE | 2024-12-21 12:59:52.097Z | 128.14° SE | 26.75° | 2024-12-22 11:35:52.097Z | 106.169° ESE |
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