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). Payloads include a variety of satellites, spacecraft, and rockets 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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2754 intel report (Beta)
OPS 0100 (TRANSIT 15) details
Identifier | |
Orbit | LEO |
Last TLE update | 11 hours ago |
Origin | |
Manufacturer | APL |
Mission | Defense Navigation |
Bus & Motor | TRANSIT 5, Unknown motor |
Mass | ~50 kg wet, ~50 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Oct Cyl + 4 Pan + 1 Rod, Unknown HBR |
Radar Cross Section | 7.565 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 11 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A 25024.54742331 .00000265 00000-0 35902-3 0 9995
2 02754 90.2119 23.5029 0019039 189.0241 284.6903 13.57246491857116
Epoch: 2025-01-24T13:08Z
Definitive object data (Epoch: 2025-01-24T13:08:17.373Z)
Latitude | 66.57471° |
Longitude | -117.19194° |
Altitude | 1,053.757 km |
Speed | 7.333 km/s |
True Right ascension | 13h 35m 57s |
True Declination | 66° 27' 14" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -6.69378° |
Longitude | -117.69336° |
Altitude | 1,035.661 km |
Speed | 7.341 km/s |
Apparent Right ascension | 13h 30m 10s |
Apparent Declination | -21° 54' 25" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 01:24:29 |
Azimuth | 355.746° N |
Elevation | -71.95° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 1,056.884 km |
Perigee altitude | 1,028.627 km |
Semi-major axis | 7,420.892 km |
Eccentricity | 0.0019039 |
Inclination | 90.2119° |
RAAN | 23.5029° |
Arg. of periapsis | 189.0241° |
True anomaly | 284.47913° |
Mean anomaly | 284.6903° |
Eccentric anomaly | 284.58473° |
Mean motion | 3.39515 °/min |
BSTAR | 0.00035902 |
Orbital period | 106.03 mins |
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Other satellites on launch #34 in the year 1967 (1967-04-14 UTC)
OPS 0100 (TRANSIT 15) Visibility forecast
Observer location: undefined°, undefined
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. |
---|---|---|---|---|---|---|---|
10 mins | 2025-01-25 01:04:43.845Z | 215.346° SW | 2025-01-25 01:09:43.845Z | 275.18° WNW | 29.776° | 2025-01-25 01:14:43.845Z | 335.216° NNW |
4 mins | 2025-01-25 10:27:43.845Z | 58.944° ENE | 2025-01-25 10:29:43.845Z | 78.401° E | 12.692° | 2025-01-25 10:31:43.845Z | 97.418° ESE |
11 mins | 2025-01-25 12:10:43.845Z | 2.045° NNE | 2025-01-25 12:15:43.845Z | 355.652° N | 44.435° | 2025-01-25 12:21:43.845Z | 185.117° SSW |
Authenticating...
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