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: 14 hours ago
TLE from 14 hours ago
0 OPS 3367 A
1 00734U 64002B 26034.28996756 .00000142 00000-0 73547-4 0 9990
2 00734 98.9749 320.3723 0013808 212.0692 147.9650 14.29659491229638Epoch: 2026-02-03T06:57Z
TLE epoch observation values (Epoch: 2026-02-03T06:57:33.197Z)
Latitude
-0.00001°
Longitude
82.51095°
Altitude
804.188 km
Speed
7.447 km/s
True Right ascension
21h 21m 29s
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
22:51:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
799.926 km
Perigee altitude
780.13 km
Semi-major axis
7,168.165 km
Eccentricity
0.00138
Inclination
98.9749°
RAAN
320.3723°
Arg. of periapsis
212.0692°
True anomaly
148.04881°
Mean anomaly
147.965°
Eccentric anomaly
148.00692°
Mean motion
3.57628 °/min
Orbital period
100.66 mins
BSTAR
0.000073547
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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 | 2026-02-04 07:04:28.550Z | 42.294° NE | 2026-02-04 07:08:28.550Z | 105.679° ESE | 26.287° | 2026-02-04 07:12:28.550Z | 157.05° SSE |
| 7 mins | 2026-02-04 08:44:28.550Z | 343.211° N | 2026-02-04 08:47:28.550Z | 293.138° NW | 27.875° | 2026-02-04 08:51:28.550Z | 234.543° WSW |
| 8 mins | 2026-02-04 18:22:28.550Z | 133.459° SE | 2026-02-04 18:25:28.550Z | 80.913° E | 35.246° | 2026-02-04 18:30:28.550Z | 359.848° N |
| 5 mins | 2026-02-04 20:03:28.550Z | 236.335° WSW | 2026-02-04 20:05:28.550Z | 266.134° W | 19.988° | 2026-02-04 20:08:28.550Z | 306.893° NW |
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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