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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2754 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A 25311.15915522 .00000192 00000-0 25572-3 0 9996
2 02754 90.2304 29.9557 0021353 78.3375 342.0848 13.57343494895994Epoch: 2025-11-07T03:49Z
TLE epoch observation values (Epoch: 2025-11-07T03:49:11.011Z)
Latitude
60.43583°
Longitude
-74.35138°
Altitude
1,040.661 km
Speed
7.345 km/s
True Right ascension
01h 58m 12s
True Declination
60° 17' 37"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
14:10:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,058.246 km
Perigee altitude
1,026.556 km
Semi-major axis
7,420.538 km
Eccentricity
0.00214
Inclination
90.2304°
RAAN
29.9557°
Arg. of periapsis
78.3375°
True anomaly
342.00934°
Mean anomaly
342.0848°
Eccentric anomaly
342.04709°
Mean motion
3.39539 °/min
Orbital period
106.03 mins
BSTAR
0.00025572
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Other satellites on launch #34 in the year 1967 (1967-04-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OPS 0100 (TRANSIT 15) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-07 18:15:27.499Z | 352.925° N | 2025-11-07 18:21:27.499Z | 285.331° WNW | 38.906° | 2025-11-07 18:27:27.499Z | 204.31° SW |
| 8 mins | 2025-11-08 04:26:27.499Z | 113.554° SE | 2025-11-08 04:30:27.499Z | 68.76° E | 20.481° | 2025-11-08 04:34:27.499Z | 28.243° NE |
| 11 mins | 2025-11-08 06:10:27.499Z | 196.306° SSW | 2025-11-08 06:15:27.499Z | 271.448° WNW | 39.893° | 2025-11-08 06:21:27.499Z | 348.403° N |
| 10 mins | 2025-11-08 17:17:27.499Z | 17.044° NNE | 2025-11-08 17:21:27.499Z | 74.328° E | 39.568° | 2025-11-08 17:27:27.499Z | 165.455° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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