OPS 9326 (IDSCS 13), 2653
Orbit data source: Space-Track
OPS 9326 (IDSCS 13), 2653 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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2653 intel report (Beta)
OPS 9326 (IDSCS 13) 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 9326 (IDSCS 13)
1 02653U 67003F 24355.27697114 -.00000097 00000-0 00000-0 0 9995
2 02653 7.1403 51.0241 0044902 49.8875 310.4341 1.07749332126838
Epoch: 2024-12-20T06:38Z
Definitive object data (Epoch: 2024-12-20T06:38:50.306Z)
Latitude | -0.00001° |
Longitude | -138.09791° |
Altitude | 33,694.789 km |
Speed | 3.159 km/s |
True Right ascension | 03h 23m 49s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 5.87486° |
Longitude | -13.0672° |
Altitude | 33,763.526 km |
Speed | 3.153 km/s |
Apparent Right ascension | 11h 44m 54s |
Apparent Declination | 0° 03' 18" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 11:37:06 |
Azimuth | 176.959° S |
Elevation | 50.099° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 33,994.116 km |
Perigee altitude | 33,633.178 km |
Semi-major axis | 40,191.784 km |
Eccentricity | 0.0044902 |
Inclination | 7.1403° |
RAAN | 51.0241° |
Arg. of periapsis | 49.8875° |
True anomaly | 310.04103° |
Mean anomaly | 310.4341° |
Eccentric anomaly | 310.23771° |
Mean motion | 0.26936 °/min |
BSTAR | Unknown |
Orbital period | 1336.49 mins |
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Other satellites on launch #3 in the year 1967 (1967-01-18 UTC)
OPS 9326 (IDSCS 13) 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. |
---|---|---|---|---|---|---|---|
1440 mins | 2024-12-21 12:35:16.752Z | 176.96° S | 2024-12-21 12:35:16.752Z | 176.96° S | 37.487° | 2024-12-22 12:35:16.752Z | 137.318° SSE |
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