OPS 3367 B, 735
Orbit data source: Space-Track
OPS 3367 B, 735 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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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 B
1 00735U 64002C 26034.34677556 .00000144 00000-0 76082-4 0 9991
2 00735 98.9819 315.1777 0016106 338.1493 21.8998 14.28542932227601Epoch: 2026-02-03T08:19Z
TLE epoch observation values (Epoch: 2026-02-03T08:19:21.408Z)
Latitude
-0.00009°
Longitude
56.80949°
Altitude
788.801 km
Speed
7.465 km/s
True Right ascension
21h 00m 42s
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
00:19:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
805.317 km
Perigee altitude
782.215 km
Semi-major axis
7,171.903 km
Eccentricity
0.00161
Inclination
98.9819°
RAAN
315.1777°
Arg. of periapsis
338.1493°
True anomaly
21.96877°
Mean anomaly
21.8998°
Eccentric anomaly
21.93427°
Mean motion
3.57348 °/min
Orbital period
100.74 mins
BSTAR
0.000076082
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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 B 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-02-04 06:45:34.943Z | 35.166° NE | 2026-02-04 06:49:34.943Z | 86.357° E | 27.904° | 2026-02-04 06:54:34.943Z | 159.539° S |
| 7 mins | 2026-02-04 08:26:34.943Z | 341.238° N | 2026-02-04 08:29:34.943Z | 291.917° WNW | 26.99° | 2026-02-04 08:33:34.943Z | 236.171° WSW |
| 8 mins | 2026-02-04 18:04:34.943Z | 138.774° SSE | 2026-02-04 18:08:34.943Z | 58.827° ENE | 36.657° | 2026-02-04 18:12:34.943Z | 359.853° N |
| 6 mins | 2026-02-04 19:45:34.943Z | 232.221° WSW | 2026-02-04 19:47:34.943Z | 258.925° W | 18.194° | 2026-02-04 19:51:34.943Z | 310.578° 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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