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: 7 hours ago
TLE from 7 hours ago
0 OPS 4947 (TRANSIT 17)
1 02965U 67092A 25289.57994444 .00000141 00000-0 19066-3 0 9999
2 02965 89.2532 28.7771 0048706 44.0107 328.7054 13.53434097863247Epoch: 2025-10-16T13:55Z
TLE epoch observation values (Epoch: 2025-10-16T13:55:07.199Z)
Latitude
12.3823°
Longitude
154.82259°
Altitude
1,030.941 km
Speed
7.352 km/s
True Right ascension
01h 55m 45s
True Declination
12° 18' 47"
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
15:12:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,092.909 km
Perigee altitude
1,020.485 km
Semi-major axis
7,434.834 km
Eccentricity
0.00487
Inclination
89.2532°
RAAN
28.7771°
Arg. of periapsis
44.0107°
True anomaly
328.41397°
Mean anomaly
328.7054°
Eccentric anomaly
328.55984°
Mean motion
3.3856 °/min
Orbital period
106.33 mins
BSTAR
0.00019066
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-17 05:57:21.040Z | 124.963° SE | 2025-10-17 06:02:21.040Z | 69.232° E | 22.557° | 2025-10-17 06:06:21.040Z | 27.491° NE |
| 10 mins | 2025-10-17 07:43:21.040Z | 205.577° SW | 2025-10-17 07:47:21.040Z | 260.53° W | 36.765° | 2025-10-17 07:53:21.040Z | 345.83° N |
| 12 mins | 2025-10-17 18:50:21.040Z | 5.443° NNE | 2025-10-17 18:56:21.040Z | 121.65° SE | 43.834° | 2025-10-17 19:02:21.040Z | 176.289° S |
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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