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 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: 15 hours ago
TLE from 15 hours ago
0 OPS 9346 (IDSCS 24)
1 03289U 68050F 26033.97620131 -.00000103 00000-0 00000-0 0 9999
2 03289 6.8022 54.5816 0044939 139.2805 229.3699 1.07287642 49211Epoch: 2026-02-02T23:25Z
TLE epoch observation values (Epoch: 2026-02-02T23:25:43.793Z)
Latitude
0.9639°
Longitude
-61.78564°
Altitude
34,044.53 km
Speed
3.136 km/s
True Right ascension
04h 11m 14s
True Declination
0° 57' 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
16:48:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,110.001 km
Perigee altitude
33,747.73 km
Semi-major axis
40,307.002 km
Eccentricity
0.00449
Inclination
6.8022°
RAAN
54.5816°
Arg. of periapsis
139.2805°
True anomaly
228.98051°
Mean anomaly
229.3699°
Eccentric anomaly
229.17506°
Mean motion
0.26821 °/min
Orbital period
1,342.24 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. |
|---|---|---|---|---|---|---|---|
| 35 mins | 2026-02-04 00:02:37.941Z | 100.107° ESE | 2026-02-04 00:22:37.941Z | 99.515° ESE | 10.016° | 2026-02-04 00:37:37.941Z | 99.089° 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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