OPS 4467 B, 813
Orbit data source: Space-Track
OPS 4467 B, 813 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: 15 hours ago
TLE from 15 hours ago
0 OPS 4467 B
1 00813U 64031B 25320.62874154 .00000218 00000-0 11929-3 0 9991
2 00813 99.8001 84.0620 0005920 56.9939 303.1805 14.23650091184686Epoch: 2025-11-16T15:05Z
TLE epoch observation values (Epoch: 2025-11-16T15:05:23.269Z)
Latitude
0.0001°
Longitude
161.77423°
Altitude
813.589 km
Speed
7.448 km/s
True Right ascension
05h 36m 14s
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
03:10:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.5 km
Perigee altitude
805.989 km
Semi-major axis
7,188.381 km
Eccentricity
0.00059
Inclination
99.8001°
RAAN
84.062°
Arg. of periapsis
56.9939°
True anomaly
303.1237°
Mean anomaly
303.1805°
Eccentric anomaly
303.1521°
Mean motion
3.5612 °/min
Orbital period
101.09 mins
BSTAR
0.00011929
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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 B 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-17 08:04:19.538Z | 154.897° SSE | 2025-11-17 08:09:19.538Z | 41.199° NE | 43.057° | 2025-11-17 08:13:19.538Z | 350.584° N |
| 6 mins | 2025-11-17 20:23:19.538Z | 60.572° ENE | 2025-11-17 20:25:19.538Z | 91.394° ESE | 22.605° | 2025-11-17 20:29:19.538Z | 146.457° SSE |
| 8 mins | 2025-11-17 22:02:19.538Z | 349.996° N | 2025-11-17 22:05:19.538Z | 296.826° NW | 32.815° | 2025-11-17 22:10:19.538Z | 224.269° SW |
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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