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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OPS 2366 (TRANSIT 14)
1 2401U 66076A 26192.13394764 .00000062 00000-0 73909-4 0 9999
2 2401 88.8450 63.0032 0030752 233.8168 292.1307 13.53960722954330Epoch: 2026-07-11T03:12Z
TLE epoch observation values (Epoch: 2026-07-11T03:12:53.076Z)
Latitude
14.34649°
Longitude
-94.5634°
Altitude
1,051.404 km
Speed
7.331 km/s
True Right ascension
16h 10m 50s
True Declination
14° 16' 03"
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
03:29:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.627 km
Perigee altitude
1,031.912 km
Semi-major axis
7,432.906 km
Eccentricity
0.00308
Inclination
88.845°
RAAN
63.0032°
Arg. of periapsis
233.8168°
True anomaly
291.8038°
Mean anomaly
292.1307°
Eccentric anomaly
291.9673°
Mean motion
3.38692 °/min
Orbital period
106.29 mins
BSTAR
0.000073909
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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 | 2026-07-11 16:41:04.781Z | 209.626° SW | 2026-07-11 16:47:04.781Z | 276.527° WNW | 32.007° | 2026-07-11 16:53:04.781Z | 343.13° N |
| 5 mins | 2026-07-12 02:06:04.781Z | 54.592° ENE | 2026-07-12 02:08:04.781Z | 74.715° E | 14.802° | 2026-07-12 02:11:04.781Z | 103.853° ESE |
| 11 mins | 2026-07-12 03:50:04.781Z | 357.501° N | 2026-07-12 03:55:04.781Z | 285.982° WNW | 44.56° | 2026-07-12 04:01:04.781Z | 187.571° 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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