Showing default

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.

Loading next visibility...
Identifier
2965, 1967-092A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
1967-09-25 (58 years ago)
Launch vehicle
SCOUT A
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 OPS 4947 (TRANSIT 17)
1  2965U 67092A   26061.80206525  .00000164  00000-0  22563-3 0  9991
2  2965  89.2554  18.3348 0048070   5.9572  54.7732 13.53475855881800
Epoch: 2026-03-02T19:14Z
TLE epoch observation values (Epoch: 2026-03-02T19:14:58.437Z)
Latitude
61.26176°
Longitude
-69.64785°
Altitude
1,049.539 km
Speed
7.343 km/s
True Right ascension
01h 18m 44s
True Declination
61° 07' 20"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
05:28:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,092.282 km
Perigee altitude
1,020.805 km
Semi-major axis
7,434.681 km
Eccentricity
0.00481
Inclination
89.2554°
RAAN
18.3348°
Arg. of periapsis
5.9572°
True anomaly
55.22473°
Mean anomaly
54.7732°
Eccentric anomaly
54.99881°
Mean motion
3.38571 °/min
Orbital period
106.33 mins
BSTAR
0.00022563
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|