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
Defense Weather
Bus & Motor
P35, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 0.3 m
Radar Cross Section
0.377 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OPS 3367 B
1 00735U 64002C 25258.56144501 .00000082 00000-0 51605-4 0 9996
2 00735 98.9753 170.3532 0017007 25.8785 334.3242 14.28474301207508Epoch: 2025-09-15T13:28Z
TLE epoch observation values (Epoch: 2025-09-15T13:28:28.848Z)
Latitude
-0.00008°
Longitude
-26.53132°
Altitude
788.757 km
Speed
7.465 km/s
True Right ascension
11h 21m 24s
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
17:14:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
806.193 km
Perigee altitude
781.798 km
Semi-major axis
7,172.132 km
Eccentricity
0.0017
Inclination
98.9753°
RAAN
170.3532°
Arg. of periapsis
25.8785°
True anomaly
334.2396°
Mean anomaly
334.3242°
Eccentric anomaly
334.28192°
Mean motion
3.57331 °/min
Orbital period
100.75 mins
BSTAR
0.000051605
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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 | 2025-09-16 06:51:55.864Z | 22.486° NNE | 2025-09-16 06:55:55.864Z | 79.189° E | 41.217° | 2025-09-16 07:00:55.864Z | 182.123° SSW |
| 4 mins | 2025-09-16 08:33:55.864Z | 317.444° NNW | 2025-09-16 08:34:55.864Z | 304.101° NW | 16.066° | 2025-09-16 08:37:55.864Z | 265.893° W |
| 8 mins | 2025-09-16 18:10:55.864Z | 166.475° S | 2025-09-16 18:13:55.864Z | 175.696° S | 43.873° | 2025-09-16 18:18:55.864Z | 345.288° N |
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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