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 | 15 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 15 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A 24356.63508083 .00000178 00000-0 23743-3 0 9999
2 02754 90.2117 22.7774 0017654 296.2327 179.0108 13.57229998852515Epoch: 2024-12-21T15:14Z
Definitive object data (Epoch: 2024-12-21T15:14:30.983Z)
| Latitude | 64.83444° |
| Longitude | -116.08683° |
| Altitude | 1,070.156 km |
| Speed | 7.316 km/s |
| True Right ascension | 13h 32m 54s |
| True Declination | 64° 42' 27" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -75.84594° |
| Longitude | -117.35692° |
| Altitude | 1,063.067 km |
| Speed | 7.325 km/s |
| Apparent Right ascension | 16h 13m 03s |
| Apparent Declination | -61° 29' 18" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:09:58 |
| Azimuth | 162.713° S |
| Elevation | -66.739° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,055.916 km |
| Perigee altitude | 1,029.714 km |
| Semi-major axis | 7,420.952 km |
| Eccentricity | 0.0017654 |
| Inclination | 90.2117° |
| RAAN | 22.7774° |
| Arg. of periapsis | 296.2327° |
| True anomaly | 179.01428° |
| Mean anomaly | 179.0108° |
| Eccentric anomaly | 179.01254° |
| Mean motion | 3.39511 °/min |
| BSTAR | 0.00023743 |
| 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-22 12:33:16.855Z | 57.57° ENE | 2024-12-22 12:35:16.855Z | 76.042° E | 11.752° | 2024-12-22 12:37:16.855Z | 94.352° ESE |
| 11 mins | 2024-12-22 14:17:16.855Z | 4.668° NNE | 2024-12-22 14:22:16.855Z | 146.368° SSE | 44.671° | 2024-12-22 14:28:16.855Z | 181.877° SSW |
| 4 mins | 2024-12-22 16:05:16.855Z | 307.106° NW | 2024-12-22 16:07:16.855Z | 286.959° WNW | 14.279° | 2024-12-22 16:09:16.855Z | 267.547° W |
| 11 mins | 2024-12-23 02:10:16.855Z | 170.442° S | 2024-12-23 02:15:16.855Z | 115.959° SE | 44.474° | 2024-12-23 02:21:16.855Z | 0.184° NNE |
| 5 mins | 2024-12-23 04:00:16.855Z | 264.309° W | 2024-12-23 04:02:16.855Z | 284.645° WNW | 14.558° | 2024-12-23 04:05:16.855Z | 313.362° NW |
Authenticating...
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