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: 12 hours ago
TLE from 12 hours ago
0 OPS 4947 (TRANSIT 17)
1 2965U 67092A 25333.73938588 .00000124 00000-0 16756-3 0 9998
2 2965 89.2512 25.4263 0045688 273.6315 212.7430 13.53448787869216Epoch: 2025-11-29T17:44Z
TLE epoch observation values (Epoch: 2025-11-29T17:44:42.940Z)
Latitude
53.99448°
Longitude
-130.64115°
Altitude
1,097.179 km
Speed
7.295 km/s
True Right ascension
13h 37m 36s
True Declination
53° 50' 18"
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
02:58:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,090.611 km
Perigee altitude
1,022.675 km
Semi-major axis
7,434.78 km
Eccentricity
0.00457
Inclination
89.2512°
RAAN
25.4263°
Arg. of periapsis
273.6315°
True anomaly
212.46118°
Mean anomaly
212.743°
Eccentric anomaly
212.60196°
Mean motion
3.38564 °/min
Orbital period
106.33 mins
BSTAR
0.00016756
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-30 05:40:59.215Z | 247.935° W | 2025-11-30 05:44:59.215Z | 285.816° WNW | 15.792° | 2025-11-30 05:47:59.215Z | 314.83° NW |
| 10 mins | 2025-11-30 15:01:59.215Z | 28.015° NE | 2025-11-30 15:05:59.215Z | 78.209° E | 30.155° | 2025-11-30 15:11:59.215Z | 146.943° SSE |
| 10 mins | 2025-11-30 16:47:59.215Z | 337.488° NNW | 2025-11-30 16:52:59.215Z | 271.53° WNW | 30.591° | 2025-11-30 16:57:59.215Z | 218.92° SW |
| 9 mins | 2025-12-01 02:57:59.215Z | 128.531° SE | 2025-12-01 03:01:59.215Z | 80.984° E | 27.555° | 2025-12-01 03:06:59.215Z | 23.368° NE |
| 10 mins | 2025-12-01 04:43:59.215Z | 214.925° SW | 2025-12-01 04:47:59.215Z | 268.913° W | 33.491° | 2025-12-01 04:53:59.215Z | 342.541° N |
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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