OPS 9341 (IDSCS 19), 3284
Orbit data source: Space-Track
OPS 9341 (IDSCS 19), 3284 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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3284 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 9341 (IDSCS 19)
1 03284U 68050A 25258.71086398 -.00000069 00000-0 00000-0 0 9996
2 03284 6.6496 54.1762 0015087 145.4196 224.7328 1.07853722 47257Epoch: 2025-09-15T17:03Z
TLE epoch observation values (Epoch: 2025-09-15T17:03:38.647Z)
Latitude
1.14049°
Longitude
173.30935°
Altitude
33,828.991 km
Speed
3.147 km/s
True Right ascension
04h 16m 31s
True Declination
1° 08' 21"
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
11:33:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,848.312 km
Perigee altitude
33,727.115 km
Semi-major axis
40,165.851 km
Eccentricity
0.00151
Inclination
6.6496°
RAAN
54.1762°
Arg. of periapsis
145.4196°
True anomaly
224.61129°
Mean anomaly
224.7328°
Eccentric anomaly
224.67203°
Mean motion
0.26962 °/min
Orbital period
1,335.2 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 9341 (IDSCS 19) 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 | 2025-09-16 18:50:31.300Z | 248.659° W | 2025-09-17 18:50:31.300Z | 220.448° SW | 34.442° | 2025-09-17 18:50:31.300Z | 220.448° SW |
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3284 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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