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: 9 hours ago
TLE from 9 hours ago
0 OPS 3367 A
1 00734U 64002B 26120.51201389 .00000099 00000-0 56888-4 0 9993
2 00734 98.9787 49.2035 0013919 328.9545 31.0813 14.29689273241954Epoch: 2026-04-30T12:17Z
TLE epoch observation values (Epoch: 2026-04-30T12:17:18.000Z)
Latitude
0.00009°
Longitude
6.42093°
Altitude
787.142 km
Speed
7.465 km/s
True Right ascension
03h 16m 48s
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
04:48:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
799.906 km
Perigee altitude
779.951 km
Semi-major axis
7,168.065 km
Eccentricity
0.00139
Inclination
98.9787°
RAAN
49.2035°
Arg. of periapsis
328.9545°
True anomaly
31.16377°
Mean anomaly
31.0813°
Eccentric anomaly
31.12252°
Mean motion
3.57635 °/min
Orbital period
100.66 mins
BSTAR
0.000056888
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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 | 2026-05-01 07:21:22.653Z | 38.503° NE | 2026-05-01 07:25:22.653Z | 96.882° ESE | 27.712° | 2026-05-01 07:29:22.653Z | 155.539° SSE |
| 7 mins | 2026-05-01 09:01:22.653Z | 345.794° N | 2026-05-01 09:04:22.653Z | 301.945° NW | 27.078° | 2026-05-01 09:08:22.653Z | 238.694° WSW |
| 8 mins | 2026-05-01 18:39:22.653Z | 137.493° SSE | 2026-05-01 18:43:22.653Z | 59.269° ENE | 35.937° | 2026-05-01 18:47:22.653Z | 0.532° NNE |
| 6 mins | 2026-05-01 20:20:22.653Z | 232.431° WSW | 2026-05-01 20:22:22.653Z | 260.038° W | 18.834° | 2026-05-01 20:26:22.653Z | 311.856° 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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