OPS 9332 (IDSCS 17), 2863
Orbit data source: Space-Track
OPS 9332 (IDSCS 17), 2863 is a payload satellite owned by SAMSO (US) in GEO that was launched on Sat, 01 Jul 1967 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft 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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2863 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
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
Shape & HBR
Poly, 0.5 m
Radar Cross Section
0.926 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 OPS 9332 (IDSCS 17)
1 02863U 67066B 25261.17544793 -.00000068 00000-0 00000-0 0 9995
2 02863 2.2250 103.1072 0060316 228.4859 263.9971 1.09896590121738Epoch: 2025-09-18T04:12Z
TLE epoch observation values (Epoch: 2025-09-18T04:12:38.701Z)
Latitude
1.68192°
Longitude
174.41954°
Altitude
33,313.74 km
Speed
3.168 km/s
True Right ascension
15h 39m 41s
True Declination
1° 40' 48"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:19:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,527.696 km
Perigee altitude
33,049.19 km
Semi-major axis
39,666.58 km
Eccentricity
0.00603
Inclination
2.225°
RAAN
103.1072°
Arg. of periapsis
228.4859°
True anomaly
263.31028°
Mean anomaly
263.9971°
Eccentric anomaly
263.65363°
Mean motion
0.27473 °/min
Orbital period
1,310.38 mins
BSTAR
0
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Other satellites on launch #66 in the year 1967 (1967-07-01 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OPS 9332 (IDSCS 17) Visibility forecast
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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 | 2025-09-19 02:26:47.177Z | 241.489° WSW | 2025-09-20 00:31:47.177Z | 205.425° SW | 33.676° | 2025-09-20 02:26:47.177Z | 200.76° SSW |
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2863 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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