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 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 9333 (IDSCS 18)
1 02864U 67066C 25259.92254154 -.00000122 00000-0 00000-0 0 9996
2 02864 2.1565 104.7507 0057507 220.0038 272.4978 1.09786246128546Epoch: 2025-09-16T22:08Z
TLE epoch observation values (Epoch: 2025-09-16T22:08:27.589Z)
Latitude
1.62795°
Longitude
-91.60984°
Altitude
33,305.178 km
Speed
3.17 km/s
True Right ascension
15h 46m 26s
True Declination
1° 37' 34"
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
17:03:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,543.28 km
Perigee altitude
33,086.753 km
Semi-major axis
39,693.153 km
Eccentricity
0.00575
Inclination
2.1565°
RAAN
104.7507°
Arg. of periapsis
220.0038°
True anomaly
271.83925°
Mean anomaly
272.4978°
Eccentric anomaly
272.16855°
Mean motion
0.27445 °/min
Orbital period
1,311.69 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. |
|---|---|---|---|---|---|---|---|
| 499 mins | 2025-09-18 00:14:49.010Z | 117.902° SE | 2025-09-18 00:14:49.010Z | 117.902° SE | 18.358° | 2025-09-18 08:33:49.010Z | 108.049° 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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