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
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: 8 hours ago
TLE from 8 hours ago
0 OPS 3367 A
1 00734U 64002B 25258.61409823 .00000090 00000-0 53363-4 0 9994
2 00734 98.9647 175.5346 0013373 263.8927 96.0730 14.29584172209531Epoch: 2025-09-15T14:44Z
TLE epoch observation values (Epoch: 2025-09-15T14:44:18.087Z)
Latitude
-0.00003°
Longitude
-40.35698°
Altitude
797.068 km
Speed
7.455 km/s
True Right ascension
11h 42m 08s
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
15:17:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
799.866 km
Perigee altitude
780.693 km
Semi-major axis
7,168.416 km
Eccentricity
0.00134
Inclination
98.9647°
RAAN
175.5346°
Arg. of periapsis
263.8927°
True anomaly
96.22536°
Mean anomaly
96.073°
Eccentric anomaly
96.14918°
Mean motion
3.57609 °/min
Orbital period
100.67 mins
BSTAR
0.000053363
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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 | 2025-09-16 06:27:39.070Z | 48.218° ENE | 2025-09-16 06:30:39.070Z | 88.044° E | 21.525° | 2025-09-16 06:34:39.070Z | 143.384° SSE |
| 7 mins | 2025-09-16 08:07:39.070Z | 348.317° N | 2025-09-16 08:10:39.070Z | 290.657° WNW | 33.341° | 2025-09-16 08:14:39.070Z | 225.993° WSW |
| 7 mins | 2025-09-16 17:45:39.070Z | 123.591° SE | 2025-09-16 17:48:39.070Z | 75.364° E | 29.921° | 2025-09-16 17:52:39.070Z | 9.549° NNE |
| 7 mins | 2025-09-16 19:25:39.070Z | 219.465° SW | 2025-09-16 19:28:39.070Z | 268.124° W | 24.733° | 2025-09-16 19:32:39.070Z | 320.562° 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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