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: 21 hours ago
TLE from 21 hours ago
0 OPS 4467 B
1 00813U 64031B 25306.22122706 .00000114 00000-0 73416-4 0 9995
2 00813 99.7987 68.0266 0006105 92.5140 267.6734 14.23642358182637Epoch: 2025-11-02T05:18Z
TLE epoch observation values (Epoch: 2025-11-02T05:18:34.017Z)
Latitude
-0.00003°
Longitude
-53.3552°
Altitude
816.124 km
Speed
7.445 km/s
True Right ascension
04h 32m 06s
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
22:28:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.659 km
Perigee altitude
805.881 km
Semi-major axis
7,188.407 km
Eccentricity
0.00061
Inclination
99.7987°
RAAN
68.0266°
Arg. of periapsis
92.514°
True anomaly
267.6035°
Mean anomaly
267.6734°
Eccentric anomaly
267.63845°
Mean motion
3.56118 °/min
Orbital period
101.09 mins
BSTAR
0.000073416
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-03 06:46:40.932Z | 97.115° ESE | 2025-11-03 06:49:40.932Z | 61.155° ENE | 16.206° | 2025-11-03 06:52:40.932Z | 24.616° NE |
| 8 mins | 2025-11-03 08:25:40.932Z | 180.138° SSW | 2025-11-03 08:28:40.932Z | 235.661° WSW | 41.76° | 2025-11-03 08:33:40.932Z | 337.729° N |
| 8 mins | 2025-11-03 20:42:40.932Z | 39.391° NE | 2025-11-03 20:45:40.932Z | 96.898° ESE | 34.644° | 2025-11-03 20:50:40.932Z | 171.802° S |
| 6 mins | 2025-11-03 22:22:40.932Z | 335.242° NNW | 2025-11-03 22:25:40.932Z | 290.074° WNW | 21.772° | 2025-11-03 22:28:40.932Z | 250.709° W |
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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