CTC-0, 62401
Orbit data source: Space-Track
CTC-0, 62401 is an American payload satellite in LEO that was launched on Sat, 21 Dec 2024 UTC via an FALCON 9 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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62401 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
Manufacturer
Endurosat
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
9.75 kg wet, 9.75 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.154 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 CTC-0
1 62401U 24247AA 26221.64084907 .00014559 00000-0 34896-3 0 9990
2 62401 44.9732 332.4241 0007342 263.2166 96.7886 15.41336873 91460Epoch: 2026-08-09T15:22Z
TLE epoch observation values (Epoch: 2026-08-09T15:22:49.359Z)
Latitude
-0.00007°
Longitude
143.58344°
Altitude
442.754 km
Speed
7.648 km/s
True Right ascension
22h 09m 41s
True Declination
0° 00' 00"
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
22:55:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.795 km
Perigee altitude
438.777 km
Semi-major axis
6,821.923 km
Eccentricity
0.00073
Inclination
44.9732°
RAAN
332.4241°
Arg. of periapsis
263.2166°
True anomaly
96.87213°
Mean anomaly
96.7886°
Eccentric anomaly
96.83037°
Mean motion
3.85197 °/min
Orbital period
93.46 mins
BSTAR
0.00034896
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Other satellites on launch #247 in the year 2024 (2024-12-21 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.CTC-0 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-10 10:13:40.608Z | 206.801° SW | 2026-08-10 10:16:40.608Z | 145.707° SSE | 26.284° | 2026-08-10 10:19:40.608Z | 84.068° E |
| 5 mins | 2026-08-10 11:52:40.608Z | 269.863° W | 2026-08-10 11:54:40.608Z | 5.053° NNE | 40.127° | 2026-08-10 11:57:40.608Z | 62.03° ENE |
| 5 mins | 2026-08-10 13:30:40.608Z | 304.434° NW | 2026-08-10 13:32:40.608Z | 0.23° NNE | 29.512° | 2026-08-10 13:35:40.608Z | 65.764° ENE |
| 5 mins | 2026-08-10 15:08:40.608Z | 302.943° NW | 2026-08-10 15:10:40.608Z | 356.557° N | 39.927° | 2026-08-10 15:13:40.608Z | 96.277° ESE |
| 5 mins | 2026-08-10 16:46:40.608Z | 265.625° W | 2026-08-10 16:48:40.608Z | 213.899° SW | 26.776° | 2026-08-10 16:51:40.608Z | 152.373° SSE |
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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