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: 7 hours ago
TLE from 7 hours ago
0 OPS 2366 (TRANSIT 14)
1 02401U 66076A 26254.21252692 .00000069 00000-0 82581-4 0 9993
2 02401 88.8448 55.7104 0034126 57.2330 116.5299 13.53969716962737Epoch: 2026-09-11T05:06Z
TLE epoch observation values (Epoch: 2026-09-11T05:06:02.325Z)
Latitude
5.80636°
Longitude
168.84471°
Altitude
1,071.486 km
Speed
7.311 km/s
True Right ascension
15h 42m 22s
True Declination
5° 46' 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
04:28:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,080.102 km
Perigee altitude
1,029.371 km
Semi-major axis
7,432.873 km
Eccentricity
0.00341
Inclination
88.8448°
RAAN
55.7104°
Arg. of periapsis
57.233°
True anomaly
116.87911°
Mean anomaly
116.5299°
Eccentric anomaly
116.70457°
Mean motion
3.38694 °/min
Orbital period
106.29 mins
BSTAR
0.000082581
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-09-11 22:35:37.725Z | 18.743° NNE | 2026-09-11 22:39:37.725Z | 72.071° E | 48.225° | 2026-09-11 22:45:37.725Z | 157.59° S |
| 8 mins | 2026-09-12 00:22:37.725Z | 324.153° NNW | 2026-09-12 00:25:37.725Z | 289.385° WNW | 25.771° | 2026-09-12 00:30:37.725Z | 234.048° WSW |
| 10 mins | 2026-09-12 10:31:37.725Z | 139.971° SSE | 2026-09-12 10:35:37.725Z | 85.15° E | 40.524° | 2026-09-12 10:41:37.725Z | 14.558° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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