OPS 2366 (TRANSIT 14), 2401
Orbit data source: Space-Track
OPS 2366 (TRANSIT 14), 2401 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Thu, 18 Aug 1966 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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2401 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
~49 kg wet, ~49 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: 16 hours ago
TLE from 16 hours ago
0 OPS 2366 (TRANSIT 14)
1 2401U 66076A 25322.39684617 .00000199 00000-0 27506-3 0 9992
2 2401 88.8459 90.5307 0032349 193.9344 227.9852 13.53897749922575Epoch: 2025-11-18T09:31Z
TLE epoch observation values (Epoch: 2025-11-18T09:31:27.509Z)
Latitude
61.7109°
Longitude
-107.88329°
Altitude
1,084.744 km
Speed
7.308 km/s
True Right ascension
06h 10m 39s
True Declination
61° 34' 24"
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
22:23:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.045 km
Perigee altitude
1,030.955 km
Semi-major axis
7,433.137 km
Eccentricity
0.00323
Inclination
88.8459°
RAAN
90.5307°
Arg. of periapsis
193.9344°
True anomaly
227.71053°
Mean anomaly
227.9852°
Eccentric anomaly
227.84779°
Mean motion
3.38676 °/min
Orbital period
106.3 mins
BSTAR
0.00027506
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Other satellites on launch #76 in the year 1966 (1966-08-18 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 2366 (TRANSIT 14) 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 | 2025-11-19 08:22:49.665Z | 149.069° SSE | 2025-11-19 08:28:49.665Z | 79.042° E | 34.434° | 2025-11-19 08:34:49.665Z | 13.191° NNE |
| 10 mins | 2025-11-19 10:10:49.665Z | 227.392° WSW | 2025-11-19 10:14:49.665Z | 273.479° WNW | 26.523° | 2025-11-19 10:20:49.665Z | 338.019° N |
| 7 mins | 2025-11-19 19:32:49.665Z | 41.224° NE | 2025-11-19 19:35:49.665Z | 72.756° E | 18.697° | 2025-11-19 19:39:49.665Z | 115.682° SE |
| 11 mins | 2025-11-19 21:17:49.665Z | 351.504° N | 2025-11-19 21:22:49.665Z | 284.651° WNW | 41.438° | 2025-11-19 21:28:49.665Z | 197.392° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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