OPS 4467 A, 812
Orbit data source: Space-Track
OPS 4467 A, 812 is an American payload satellite in SSO that was launched on Thu, 18 Jun 1964 UTC via a THOR SLV-2 AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
P35, Unknown motor
Mass
50 kg wet, 50 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 4467 A
1 00812U 64031A 25306.31894046 .00000129 00000-0 78752-4 0 9991
2 00812 99.7911 70.5088 0005590 11.7251 348.4054 14.24518320183991Epoch: 2025-11-02T07:39Z
TLE epoch observation values (Epoch: 2025-11-02T07:39:16.455Z)
Latitude
0°
Longitude
-86.14614°
Altitude
809.06 km
Speed
7.451 km/s
True Right ascension
04h 42m 02s
True Declination
0° 00' 00"
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
20:55:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
811.337 km
Perigee altitude
803.303 km
Semi-major axis
7,185.457 km
Eccentricity
0.00056
Inclination
99.7911°
RAAN
70.5088°
Arg. of periapsis
11.7251°
True anomaly
348.39252°
Mean anomaly
348.4054°
Eccentric anomaly
348.39896°
Mean motion
3.56338 °/min
Orbital period
101.03 mins
BSTAR
0.000078752
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Other satellites on launch #31 in the year 1964 (1964-06-18 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 4467 A 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-03 07:23:39.760Z | 120.644° SE | 2025-11-03 07:27:39.760Z | 65.052° ENE | 25.919° | 2025-11-03 07:31:39.760Z | 9.826° NNE |
| 8 mins | 2025-11-03 09:03:39.760Z | 203.379° SW | 2025-11-03 09:07:39.760Z | 271.011° WNW | 29.291° | 2025-11-03 09:11:39.760Z | 324.455° NNW |
| 9 mins | 2025-11-03 21:19:39.760Z | 18.319° NNE | 2025-11-03 21:23:39.760Z | 119.944° SE | 44.614° | 2025-11-03 21:28:39.760Z | 192.493° SSW |
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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