OPS 9333 (IDSCS 18), 2864
Orbit data source: Space-Track
OPS 9333 (IDSCS 18), 2864 is a payload satellite owned by SAMSO (US) in GEO that was launched on Sat, 01 Jul 1967 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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2864 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Philco-Ford WDL
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: 1 day ago
TLE from 1 day ago
0 OPS 9333 (IDSCS 18)
1 2864U 67066C 25312.41805668 -.00000102 00000-0 00000+0 0 9999
2 2864 2.2770 102.7397 0058422 222.3082 140.5754 1.09785889129125Epoch: 2025-11-08T10:02Z
TLE epoch observation values (Epoch: 2025-11-08T10:02:00.097Z)
Latitude
0.13055°
Longitude
-92.33083°
Altitude
33,492.043 km
Speed
3.155 km/s
True Right ascension
07h 04m 04s
True Declination
0° 07' 49"
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
11:34:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,546.998 km
Perigee altitude
33,083.206 km
Semi-major axis
39,693.239 km
Eccentricity
0.00584
Inclination
2.277°
RAAN
102.7397°
Arg. of periapsis
222.3082°
True anomaly
140.99816°
Mean anomaly
140.5754°
Eccentric anomaly
140.78702°
Mean motion
0.27445 °/min
Orbital period
1,311.7 mins
BSTAR
0
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Other satellites on launch #66 in the year 1967 (1967-07-01 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 9333 (IDSCS 18) 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. |
|---|---|---|---|---|---|---|---|
| 367 mins | 2025-11-09 15:18:51.428Z | 113.894° SE | 2025-11-09 15:18:51.428Z | 113.894° SE | 18.696° | 2025-11-09 21:25:51.428Z | 109.408° ESE |
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2864 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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