OPS 3367 A, 734
Orbit data source: Space-Track
OPS 3367 A, 734 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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734 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: 1 day ago
TLE from 1 day ago
0 OPS 3367 A
1 734U 64002B 25289.47949058 .00000193 00000-0 93636-4 0 9992
2 734 98.9662 207.2966 0014522 170.1606 189.9862 14.29601901213948Epoch: 2025-10-16T11:30Z
TLE epoch observation values (Epoch: 2025-10-16T11:30:27.986Z)
Latitude
-0°
Longitude
9.44137°
Altitude
806.24 km
Speed
7.445 km/s
True Right ascension
13h 49m 11s
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
10:21:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
800.63 km
Perigee altitude
779.81 km
Semi-major axis
7,168.357 km
Eccentricity
0.00145
Inclination
98.9662°
RAAN
207.2966°
Arg. of periapsis
170.1606°
True anomaly
189.95739°
Mean anomaly
189.9862°
Eccentric anomaly
189.97179°
Mean motion
3.57613 °/min
Orbital period
100.67 mins
BSTAR
0.000093636
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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 A 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-17 17:52:26.879Z | 131.278° SE | 2025-10-17 17:56:26.879Z | 73.096° E | 30.997° | 2025-10-17 18:00:26.879Z | 7.871° NNE |
| 7 mins | 2025-10-17 19:33:26.879Z | 221.918° SW | 2025-10-17 19:36:26.879Z | 269.896° W | 23.69° | 2025-10-17 19:40:26.879Z | 320.399° NNW |
| 8 mins | 2025-10-18 07:46:26.879Z | 6.594° NNE | 2025-10-18 07:49:26.879Z | 314.351° NW | 43.295° | 2025-10-18 07:54:26.879Z | 203.347° 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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