OPS 9331 (IDSCS 16), 2862
Orbit data source: Space-Track
OPS 9331 (IDSCS 16), 2862 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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2862 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: 9 hours ago
TLE from 9 hours ago
0 OPS 9331 (IDSCS 16)
1 02862U 67066A 25259.20503955 -.00000122 00000-0 00000-0 0 9991
2 02862 2.2354 103.8385 0061736 230.7397 343.9710 1.09956065134183Epoch: 2025-09-16T04:55Z
TLE epoch observation values (Epoch: 2025-09-16T04:55:15.417Z)
Latitude
-1.26025°
Longitude
-110.88499°
Altitude
33,036.805 km
Speed
3.19 km/s
True Right ascension
21h 13m 18s
True Declination
-1° 15' 32"
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
06:08:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,518.936 km
Perigee altitude
33,029.342 km
Semi-major axis
39,652.276 km
Eccentricity
0.00617
Inclination
2.2354°
RAAN
103.8385°
Arg. of periapsis
230.7397°
True anomaly
343.7742°
Mean anomaly
343.971°
Eccentric anomaly
343.87275°
Mean motion
0.27488 °/min
Orbital period
1,309.67 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 9331 (IDSCS 16) 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 | 2025-09-16 13:26:24.967Z | 168.572° S | 2025-09-16 17:25:24.967Z | 160.204° S | 34.673° | 2025-09-17 13:26:24.967Z | 124.653° SE |
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2862 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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