OPS 9344 (IDSCS 22), 3287
Orbit data source: Space-Track
OPS 9344 (IDSCS 22), 3287 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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3287 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: 2 days ago
TLE from 2 days ago
0 OPS 9344 (IDSCS 22)
1 03287U 68050D 25254.63443691 -.00000056 00000-0 00000-0 0 9995
2 03287 6.6106 54.8098 0026903 139.0938 182.1850 1.07639673224261Epoch: 2025-09-11T15:13Z
TLE epoch observation values (Epoch: 2025-09-11T15:13:35.349Z)
Latitude
-4.1415°
Longitude
156.95239°
Altitude
33,948.424 km
Speed
3.14 km/s
True Right ascension
01h 04m 58s
True Declination
-4° 08' 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
23:31:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,949.143 km
Perigee altitude
33,732.74 km
Semi-major axis
40,219.079 km
Eccentricity
0.00269
Inclination
6.6106°
RAAN
54.8098°
Arg. of periapsis
139.0938°
True anomaly
182.17329°
Mean anomaly
182.185°
Eccentric anomaly
182.17914°
Mean motion
0.26909 °/min
Orbital period
1,337.85 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 9344 (IDSCS 22) 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 | 2025-09-13 07:02:05.955Z | 240.509° WSW | 2025-09-13 21:49:05.955Z | 234.683° WSW | 29.375° | 2025-09-14 07:02:05.955Z | 214.877° SW |
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3287 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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