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 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: 17 hours ago
TLE from 17 hours ago
0 OPS 9341 (IDSCS 19)
1 03284U 68050A 25302.24159324 -.00000096 00000-0 00000-0 0 9994
2 03284 6.7409 53.7979 0015263 151.2676 201.6006 1.07854655 47715Epoch: 2025-10-29T05:47Z
TLE epoch observation values (Epoch: 2025-10-29T05:47:53.655Z)
Latitude
-0.83783°
Longitude
-78.17213°
Altitude
33,843.238 km
Speed
3.146 km/s
True Right ascension
03h 06m 28s
True Declination
0° 50' 13"
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
18:02:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,848.786 km
Perigee altitude
33,726.177 km
Semi-major axis
40,165.618 km
Eccentricity
0.00153
Inclination
6.7409°
RAAN
53.7979°
Arg. of periapsis
151.2676°
True anomaly
201.53633°
Mean anomaly
201.6006°
Eccentric anomaly
201.56845°
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. |
|---|---|---|---|---|---|---|---|
| 1010 mins | 2025-10-29 22:28:27.886Z | 126.612° SE | 2025-10-30 07:39:27.886Z | 109.168° ESE | 19.303° | 2025-10-30 15:18:27.886Z | 106.065° 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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