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 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 9342 (IDSCS 20)
1 03285U 68050B 25257.74530743 -.00000094 00000-0 00000-0 0 9995
2 03285 6.6730 54.2446 0016936 144.9432 88.4852 1.07819060225195Epoch: 2025-09-14T17:53Z
TLE epoch observation values (Epoch: 2025-09-14T17:53:14.561Z)
Latitude
-5.35944°
Longitude
25.40326°
Altitude
33,794.09 km
Speed
3.15 km/s
True Right ascension
19h 10m 41s
True Declination
-5° 21' 14"
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
20:32:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,864.36 km
Perigee altitude
33,728.281 km
Semi-major axis
40,174.458 km
Eccentricity
0.00169
Inclination
6.673°
RAAN
54.2446°
Arg. of periapsis
144.9432°
True anomaly
88.67921°
Mean anomaly
88.4852°
Eccentric anomaly
88.58221°
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
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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. |
|---|---|---|---|---|---|---|---|
| OPS 9342 (IDSCS 20) is likely not visible in the next few days. |
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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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