OPS 9346 (IDSCS 24), 3289
Orbit data source: Space-Track
OPS 9346 (IDSCS 24), 3289 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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3289 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 9346 (IDSCS 24)
1 03289U 68050F 25254.92405704 -.00000123 00000-0 00000-0 0 9997
2 03289 6.4989 55.8565 0046789 132.5702 35.4120 1.07288318 47664Epoch: 2025-09-11T22:10Z
TLE epoch observation values (Epoch: 2025-09-11T22:10:38.528Z)
Latitude
1.33085°
Longitude
-99.62719°
Altitude
33,773.147 km
Speed
3.157 km/s
True Right ascension
14h 56m 50s
True Declination
1° 19' 46"
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
23:33:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,117.29 km
Perigee altitude
33,740.106 km
Semi-major axis
40,306.835 km
Eccentricity
0.00468
Inclination
6.4989°
RAAN
55.8565°
Arg. of periapsis
132.5702°
True anomaly
35.72417°
Mean anomaly
35.412°
Eccentric anomaly
35.56793°
Mean motion
0.26821 °/min
Orbital period
1,342.23 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 9346 (IDSCS 24) 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. |
|---|---|---|---|---|---|---|---|
| 1049 mins | 2025-09-13 07:04:15.941Z | 129.608° SE | 2025-09-13 12:01:15.941Z | 119.007° SE | 26.208° | 2025-09-14 00:33:15.941Z | 116.268° SE |
| 38 mins | 2025-09-14 06:26:15.941Z | 107.969° ESE | 2025-09-14 07:04:15.941Z | 106.695° ESE | 10.39° | 2025-09-14 07:04:15.941Z | 106.695° ESE |
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3289 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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