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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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: 7 hours ago
TLE from 7 hours ago
0 OPS 3367 B
1 00735U 64002C 26177.50804487 .00000052 00000-0 39412-4 0 9996
2 00735 98.9824 102.5052 0015380 280.8234 79.1215 14.28583332248048Epoch: 2026-06-26T12:11Z
TLE epoch observation values (Epoch: 2026-06-26T12:11:35.076Z)
Latitude
-0.00006°
Longitude
4.97351°
Altitude
797.321 km
Speed
7.456 km/s
True Right ascension
06h 50m 01s
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
06:19:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
804.661 km
Perigee altitude
782.6 km
Semi-major axis
7,171.768 km
Eccentricity
0.00154
Inclination
98.9824°
RAAN
102.5052°
Arg. of periapsis
280.8234°
True anomaly
79.29464°
Mean anomaly
79.1215°
Eccentric anomaly
79.20806°
Mean motion
3.57358 °/min
Orbital period
100.74 mins
BSTAR
0.000039412
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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 | 2026-06-26 19:01:50.999Z | 168.402° S | 2026-06-26 19:05:50.999Z | 195.664° SSW | 43.968° | 2026-06-26 19:10:50.999Z | 343.899° N |
| 8 mins | 2026-06-27 07:16:50.999Z | 37.774° NE | 2026-06-27 07:20:50.999Z | 105.296° ESE | 30.637° | 2026-06-27 07:24:50.999Z | 162.038° S |
| 7 mins | 2026-06-27 08:56:50.999Z | 340.96° N | 2026-06-27 08:59:50.999Z | 296.172° NW | 24.703° | 2026-06-27 09:03:50.999Z | 240.797° WSW |
| 8 mins | 2026-06-27 18:34:50.999Z | 143.982° SSE | 2026-06-27 18:38:50.999Z | 63.106° ENE | 39.334° | 2026-06-27 18:42:50.999Z | 357.912° 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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