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: 15 hours ago
TLE from 15 hours ago
0 OPS 4947 (TRANSIT 17)
1 2965U 67092A 25319.62500833 .00000233 00000-0 32928-3 0 9998
2 2965 89.2530 26.4990 0046018 316.2171 200.1534 13.53444300867307Epoch: 2025-11-15T15:00Z
TLE epoch observation values (Epoch: 2025-11-15T15:00:00.719Z)
Latitude
23.82813°
Longitude
-73.7837°
Altitude
1,094.71 km
Speed
7.291 km/s
True Right ascension
13h 44m 40s
True Declination
23° 42' 25"
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
03:01:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,090.873 km
Perigee altitude
1,022.446 km
Semi-major axis
7,434.796 km
Eccentricity
0.0046
Inclination
89.253°
RAAN
26.499°
Arg. of periapsis
316.2171°
True anomaly
199.97269°
Mean anomaly
200.1534°
Eccentric anomaly
200.06295°
Mean motion
3.38563 °/min
Orbital period
106.33 mins
BSTAR
0.00032928
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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 | 2025-11-16 06:19:57.684Z | 237.369° WSW | 2025-11-16 06:23:57.684Z | 281.712° WNW | 21.582° | 2025-11-16 06:28:57.684Z | 331.608° NNW |
| 9 mins | 2025-11-16 15:40:57.684Z | 32.713° NE | 2025-11-16 15:44:57.684Z | 74.82° E | 23.096° | 2025-11-16 15:49:57.684Z | 129.034° SE |
| 11 mins | 2025-11-16 17:26:57.684Z | 346.818° N | 2025-11-16 17:31:57.684Z | 276.688° WNW | 38.361° | 2025-11-16 17:37:57.684Z | 204.705° SW |
| 7 mins | 2025-11-17 03:38:57.684Z | 106.464° ESE | 2025-11-17 03:41:57.684Z | 71.92° E | 20.373° | 2025-11-17 03:45:57.684Z | 31.265° NE |
| 11 mins | 2025-11-17 05:22:57.684Z | 198.132° SSW | 2025-11-17 05:27:57.684Z | 289.572° WNW | 40.15° | 2025-11-17 05:33:57.684Z | 351.024° 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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