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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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
POLY, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OPS 9346 (IDSCS 24)
1 03289U 68050F 26316.29307167 -.00000101 00000-0 00000-0 0 9997
2 03289 7.3864 51.8451 0046909 147.6551 187.1874 1.07287954 52234Epoch: 2026-11-12T07:02Z
TLE epoch observation values (Epoch: 2026-11-12T07:02:01.392Z)
Latitude
-3.12699°
Longitude
-130.14976°
Altitude
34,115.708 km
Speed
3.13 km/s
True Right ascension
01h 47m 08s
True Declination
-3° 07' 25"
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
09:10:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,117.859 km
Perigee altitude
33,739.707 km
Semi-major axis
40,306.92 km
Eccentricity
0.00469
Inclination
7.3864°
RAAN
51.8451°
Arg. of periapsis
147.6551°
True anomaly
187.12054°
Mean anomaly
187.1874°
Eccentric anomaly
187.15393°
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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-11-12 12:44:28.274Z | 213.544° SW | 2026-11-13 12:18:28.274Z | 170.551° S | 51.485° | 2026-11-13 12:44:28.274Z | 169.553° S |
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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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