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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.

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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: 7 hours ago

TLE from 7 hours ago
0 OPS 0100 (TRANSIT 15)
1  2754U 67034A   26035.06292409  .00000133  00000-0  17360-3 0  9993
2  2754  90.2262  32.0025 0019718 170.1481 257.7242 13.57372839908050
Epoch: 2026-02-04T01:30Z
TLE epoch observation values (Epoch: 2026-02-04T01:30:36.641Z)
Latitude
67.72658°
Longitude
-125.43449°
Altitude
1,060.203 km
Speed
7.326 km/s
True Right ascension
02h 05m 48s
True Declination
67° 36' 38"
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
10:08:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,056.926 km
Perigee altitude
1,027.663 km
Semi-major axis
7,420.431 km
Eccentricity
0.00197
Inclination
90.2262°
RAAN
32.0025°
Arg. of periapsis
170.1481°
True anomaly
257.50353°
Mean anomaly
257.7242°
Eccentric anomaly
257.61385°
Mean motion
3.39547 °/min
Orbital period
106.02 mins
BSTAR
0.0001736
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