OPS 3367 B, 735
Orbit data source: Space-Track
OPS 3367 B, 735 is an American payload satellite in SSO that was launched on Sun, 19 Jan 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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735 intel report (Beta)
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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 3367 B
1 00735U 64002C 25309.27294000 .00000150 00000-0 78531-4 0 9994
2 00735 98.9770 222.5036 0015572 233.7924 126.1817 14.28500443214742Epoch: 2025-11-05T06:33Z
TLE epoch observation values (Epoch: 2025-11-05T06:33:02.016Z)
Latitude
0°
Longitude
79.49722°
Altitude
806.273 km
Speed
7.447 km/s
True Right ascension
14h 50m 00s
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
19:54:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
805.076 km
Perigee altitude
782.74 km
Semi-major axis
7,172.045 km
Eccentricity
0.00156
Inclination
98.977°
RAAN
222.5036°
Arg. of periapsis
233.7924°
True anomaly
126.32556°
Mean anomaly
126.1817°
Eccentric anomaly
126.25365°
Mean motion
3.57338 °/min
Orbital period
100.75 mins
BSTAR
0.000078531
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Other satellites on launch #2 in the year 1964 (1964-01-19 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 3367 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 | 2025-11-06 06:39:57.801Z | 30.235° NE | 2025-11-06 06:44:57.801Z | 108.02° ESE | 32.518° | 2025-11-06 06:48:57.801Z | 165.549° S |
| 7 mins | 2025-11-06 08:20:57.801Z | 338.847° N | 2025-11-06 08:23:57.801Z | 295.058° NW | 22.846° | 2025-11-06 08:27:57.801Z | 242.769° WSW |
| 8 mins | 2025-11-06 17:58:57.801Z | 147.738° SSE | 2025-11-06 18:02:57.801Z | 60.58° ENE | 41.077° | 2025-11-06 18:06:57.801Z | 355.705° N |
| 4 mins | 2025-11-06 19:40:57.801Z | 245.651° WSW | 2025-11-06 19:42:57.801Z | 271.541° WNW | 15.268° | 2025-11-06 19:44:57.801Z | 296.263° NW |
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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