OPS 4947 (TRANSIT 17), 2965
Orbit data source: Space-Track
OPS 4947 (TRANSIT 17), 2965 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Mon, 25 Sep 1967 UTC via an SCOUT A 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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2965 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 OPS 4947 (TRANSIT 17)
1 02965U 67092A 25365.60351118 .00000194 00000-0 27008-3 0 9996
2 02965 89.2482 22.9954 0047700 178.9282 310.7335 13.53459006873526Epoch: 2025-12-31T14:29Z
TLE epoch observation values (Epoch: 2025-12-31T14:29:03.365Z)
Latitude
50.8426°
Longitude
-115.45721°
Altitude
1,044.722 km
Speed
7.346 km/s
True Right ascension
13h 28m 18s
True Declination
50° 40' 50"
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
19:33:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,092.069 km
Perigee altitude
1,021.142 km
Semi-major axis
7,434.742 km
Eccentricity
0.00477
Inclination
89.2482°
RAAN
22.9954°
Arg. of periapsis
178.9282°
True anomaly
310.3177°
Mean anomaly
310.7335°
Eccentric anomaly
310.52576°
Mean motion
3.38567 °/min
Orbital period
106.33 mins
BSTAR
0.00027008
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Other satellites on launch #92 in the year 1967 (1967-09-25 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 4947 (TRANSIT 17) 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-01-01 00:37:06.793Z | 127.223° SE | 2026-01-01 00:42:06.793Z | 73.622° E | 24.401° | 2026-01-01 00:47:06.793Z | 23.318° NE |
| 11 mins | 2026-01-01 02:23:06.793Z | 205.805° SW | 2026-01-01 02:28:06.793Z | 280.745° WNW | 36.919° | 2026-01-01 02:34:06.793Z | 347.195° N |
| 12 mins | 2026-01-01 13:30:06.793Z | 4.121° NNE | 2026-01-01 13:36:06.793Z | 81.57° E | 44.383° | 2026-01-01 13:42:06.793Z | 177.224° S |
| 4 mins | 2026-01-01 15:20:06.793Z | 304.561° NW | 2026-01-01 15:22:06.793Z | 283.477° WNW | 14.853° | 2026-01-01 15:24:06.793Z | 263.506° W |
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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