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: 1 day ago
TLE from 1 day ago
0 OPS 9332 (IDSCS 17)
1 02863U 67066B 25259.77213398 -.00000089 00000-0 00000-0 0 9995
2 02863 2.2218 103.1615 0060311 228.4360 68.7869 1.09896974121718Epoch: 2025-09-16T18:31Z
TLE epoch observation values (Epoch: 2025-09-16T18:31:52.375Z)
Latitude
-1.98355°
Longitude
127.12161°
Altitude
33,200.872 km
Speed
3.177 km/s
True Right ascension
02h 44m 11s
True Declination
-1° 58' 53"
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
13:39:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,527.583 km
Perigee altitude
33,049.118 km
Semi-major axis
39,666.488 km
Eccentricity
0.00603
Inclination
2.2218°
RAAN
103.1615°
Arg. of periapsis
228.436°
True anomaly
69.43293°
Mean anomaly
68.7869°
Eccentric anomaly
69.10974°
Mean motion
0.27473 °/min
Orbital period
1,310.37 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. |
|---|---|---|---|---|---|---|---|
| 333 mins | 2025-09-18 15:18:49.462Z | 250.739° W | 2025-09-18 20:51:49.462Z | 247.693° W | 17.157° | 2025-09-18 20:51:49.462Z | 247.693° W |
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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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