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: 15 hours ago
TLE from 15 hours ago
0 OPS 2366 (TRANSIT 14)
1 02401U 66076A 25308.42720323 .00000127 00000-0 16990-3 0 9991
2 02401 88.8443 92.1673 0031162 235.6457 178.5203 13.53891408920680Epoch: 2025-11-04T10:15Z
TLE epoch observation values (Epoch: 2025-11-04T10:15:10.359Z)
Latitude
54.253°
Longitude
-103.9425°
Altitude
1,090.153 km
Speed
7.301 km/s
True Right ascension
06h 15m 03s
True Declination
54° 05' 49"
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
20:42:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.186 km
Perigee altitude
1,031.86 km
Semi-major axis
7,433.16 km
Eccentricity
0.00312
Inclination
88.8443°
RAAN
92.1673°
Arg. of periapsis
235.6457°
True anomaly
178.52949°
Mean anomaly
178.5203°
Eccentric anomaly
178.5249°
Mean motion
3.38675 °/min
Orbital period
106.3 mins
BSTAR
0.0001699
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-05 09:09:16.827Z | 138.343° SSE | 2025-11-05 09:15:16.827Z | 70.851° E | 28.404° | 2025-11-05 09:20:16.827Z | 19.803° NNE |
| 10 mins | 2025-11-05 10:56:16.827Z | 215.016° SW | 2025-11-05 11:01:16.827Z | 282.488° WNW | 32.371° | 2025-11-05 11:06:16.827Z | 340.358° N |
| 5 mins | 2025-11-05 20:20:16.827Z | 57.167° ENE | 2025-11-05 20:22:16.827Z | 77.336° E | 14.446° | 2025-11-05 20:25:16.827Z | 105.608° ESE |
| 11 mins | 2025-11-05 22:04:16.827Z | 357.888° N | 2025-11-05 22:09:16.827Z | 249.254° W | 44.651° | 2025-11-05 22:15:16.827Z | 186.643° 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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