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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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: 8 hours ago
TLE from 8 hours ago
0 OPS 3367 A
1 00734U 64002B 26124.57112205 .00000103 00000-0 58709-4 0 9991
2 00734 98.9788 53.3868 0013738 316.6518 43.3581 14.29690520242538Epoch: 2026-05-04T13:42Z
TLE epoch observation values (Epoch: 2026-05-04T13:42:24.945Z)
Latitude
-0.00005°
Longitude
-14.67554°
Altitude
788.527 km
Speed
7.463 km/s
True Right ascension
03h 33m 32s
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
05:10:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
799.772 km
Perigee altitude
780.077 km
Semi-major axis
7,168.061 km
Eccentricity
0.00137
Inclination
98.9788°
RAAN
53.3868°
Arg. of periapsis
316.6518°
True anomaly
43.46632°
Mean anomaly
43.3581°
Eccentric anomaly
43.41219°
Mean motion
3.57635 °/min
Orbital period
100.66 mins
BSTAR
0.000058709
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-05 07:06:10.117Z | 46.578° ENE | 2026-05-05 07:10:10.117Z | 100.225° ESE | 20.859° | 2026-05-05 07:13:10.117Z | 139.74° SSE |
| 8 mins | 2026-05-05 08:46:10.117Z | 351.673° N | 2026-05-05 08:49:10.117Z | 299.528° NW | 34.151° | 2026-05-05 08:54:10.117Z | 221.172° SW |
| 8 mins | 2026-05-05 18:24:10.117Z | 124.234° SE | 2026-05-05 18:28:10.117Z | 57.058° ENE | 28.685° | 2026-05-05 18:32:10.117Z | 5.76° NNE |
| 7 mins | 2026-05-05 20:04:10.117Z | 215.604° SW | 2026-05-05 20:07:10.117Z | 263.209° W | 25.483° | 2026-05-05 20:11:10.117Z | 319.7° NNW |
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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