Showing default

OPS 0100 (TRANSIT 15), 2754

Orbit data source: Space-Track

OPS 0100 (TRANSIT 15), 2754 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Fri, 14 Apr 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
2754, 1967-034A
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)
1967-04-14 (59 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: 12 hours ago

TLE from 12 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A   25309.70363412  .00000167  00000-0  22029-3 0  9995
2 02754  90.2304  29.9216 0021425  82.2698  70.1028 13.57342903895799
Epoch: 2025-11-05T16:53Z
TLE epoch observation values (Epoch: 2025-11-05T16:53:13.987Z)
Latitude
27.43315°
Longitude
-88.44019°
Altitude
1,043.403 km
Speed
7.335 km/s
True Right ascension
14h 00m 09s
True Declination
27° 17' 53"
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
01:20:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,058.302 km
Perigee altitude
1,026.505 km
Semi-major axis
7,420.541 km
Eccentricity
0.00214
Inclination
90.2304°
RAAN
29.9216°
Arg. of periapsis
82.2698°
True anomaly
70.33387°
Mean anomaly
70.1028°
Eccentric anomaly
70.21831°
Mean motion
3.39539 °/min
Orbital period
106.03 mins
BSTAR
0.00022029
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
|