OPS 9342 (IDSCS 20), 3285
Orbit data source: Space-Track
OPS 9342 (IDSCS 20), 3285 is a payload satellite owned by SAMSO (US) in GEO that was launched on Thu, 13 Jun 1968 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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3285 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Philco-Ford
Mission
Non-operational spacecraft
Bus & Motor
IDCSP, Unknown motor
Mass
45 kg wet, 45 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OPS 9342 (IDSCS 20)
1 03285U 68050B 25292.41116913 -.00000114 00000-0 00000-0 0 9990
2 03285 6.7455 53.9371 0017186 149.0026 220.5817 1.07819621225571Epoch: 2025-10-19T09:52Z
TLE epoch observation values (Epoch: 2025-10-19T09:52:05.012Z)
Latitude
1.10215°
Longitude
-112.84343°
Altitude
33,847.204 km
Speed
3.146 km/s
True Right ascension
04h 13m 13s
True Declination
1° 06' 04"
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
05:33:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,865.225 km
Perigee altitude
33,727.137 km
Semi-major axis
40,174.318 km
Eccentricity
0.00172
Inclination
6.7455°
RAAN
53.9371°
Arg. of periapsis
149.0026°
True anomaly
220.4538°
Mean anomaly
220.5817°
Eccentric anomaly
220.51773°
Mean motion
0.26954 °/min
Orbital period
1,335.62 mins
BSTAR
0
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Other satellites on launch #50 in the year 1968 (1968-06-13 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 9342 (IDSCS 20) 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 | 2025-10-20 10:37:28.204Z | 147.2° SSE | 2025-10-20 11:58:28.204Z | 144.045° SSE | 35.146° | 2025-10-21 10:37:28.204Z | 115.147° SE |
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3285 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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