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 25260.10461653 -.00000105 00000-0 00000-0 0 9994
2 03284 6.6524 54.1633 0015110 145.6229 45.7144 1.07854406 47260Epoch: 2025-09-17T02:30Z
TLE epoch observation values (Epoch: 2025-09-17T02:30:38.868Z)
Latitude
-1.3027°
Longitude
-148.39883°
Altitude
33,743.845 km
Speed
3.154 km/s
True Right ascension
16h 22m 11s
True Declination
-1° 18' 05"
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
07:12:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,848.234 km
Perigee altitude
33,726.853 km
Semi-major axis
40,165.681 km
Eccentricity
0.00151
Inclination
6.6524°
RAAN
54.1633°
Arg. of periapsis
145.6229°
True anomaly
45.83851°
Mean anomaly
45.7144°
Eccentric anomaly
45.77644°
Mean motion
0.26963 °/min
Orbital period
1,335.19 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 | 2025-09-18 14:21:33.575Z | 185.093° SSW | 2025-09-18 16:49:33.575Z | 179.79° S | 37.854° | 2025-09-19 14:21:33.575Z | 140.072° SSE |
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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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