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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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
OCT CYL + 4 PAN + ANT, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 OPS 2366 (TRANSIT 14)
1 02401U 66076A 26318.72352409 .00000173 00000-0 23701-3 0 9991
2 02401 88.8534 48.1777 0031488 225.1323 287.8992 13.53982093971466Epoch: 2026-11-14T17:21Z
TLE epoch observation values (Epoch: 2026-11-14T17:21:52.481Z)
Latitude
27.34298°
Longitude
-86.70511°
Altitude
1,053.916 km
Speed
7.331 km/s
True Right ascension
15h 10m 21s
True Declination
27° 12' 31"
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
03:22:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.095 km
Perigee altitude
1,031.287 km
Semi-major axis
7,432.828 km
Eccentricity
0.00315
Inclination
88.8534°
RAAN
48.1777°
Arg. of periapsis
225.1323°
True anomaly
287.55542°
Mean anomaly
287.8992°
Eccentric anomaly
287.72735°
Mean motion
3.38698 °/min
Orbital period
106.29 mins
BSTAR
0.00023701
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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
Loading observer location...
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 | 2026-11-15 06:53:45.235Z | 191.329° SSW | 2026-11-15 06:59:45.235Z | 272.265° WNW | 64.353° | 2026-11-15 07:05:45.235Z | 351.992° N |
| 11 mins | 2026-11-15 18:02:45.235Z | 10.096° NNE | 2026-11-15 18:07:45.235Z | 76.737° E | 62.28° | 2026-11-15 18:13:45.235Z | 167.583° S |
| 7 mins | 2026-11-15 19:50:45.235Z | 317.745° NNW | 2026-11-15 19:53:45.235Z | 284.918° WNW | 20.388° | 2026-11-15 19:57:45.235Z | 244.521° WSW |
| 11 mins | 2026-11-16 05:58:45.235Z | 151.344° SSE | 2026-11-16 06:03:45.235Z | 68.891° E | 51.927° | 2026-11-16 06:09:45.235Z | 9.16° NNE |
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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