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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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: 3 days ago
TLE from 3 days ago
0 OPS 9341 (IDSCS 19)
1 03284U 68050A 26265.56013132 -.00000113 00000-0 00000-0 0 9994
2 03284 7.4061 50.7141 0014887 158.3839 238.7552 1.07854846 51269Epoch: 2026-09-22T13:26Z
TLE epoch observation values (Epoch: 2026-09-22T13:26:35.346Z)
Latitude
4.43236°
Longitude
-115.61585°
Altitude
33,816.311 km
Speed
3.148 km/s
True Right ascension
05h 49m 49s
True Declination
4° 25' 40"
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
00:42:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,847.224 km
Perigee altitude
33,727.635 km
Semi-major axis
40,165.566 km
Eccentricity
0.00149
Inclination
7.4061°
RAAN
50.7141°
Arg. of periapsis
158.3839°
True anomaly
238.60949°
Mean anomaly
238.7552°
Eccentric anomaly
238.68233°
Mean motion
0.26963 °/min
Orbital period
1,335.18 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. |
|---|---|---|---|---|---|---|---|
| 316 mins | 2026-09-25 07:26:55.701Z | 104.445° ESE | 2026-09-25 09:05:55.701Z | 101.016° ESE | 12.805° | 2026-09-25 12:42:55.701Z | 96.948° ESE |
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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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