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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CTC-0
1 62401U 24247AA 25338.52251508 .00035816 00000-0 11553-2 0 9991
2 62401 44.9764 266.5977 0004310 175.4691 184.6233 15.31598557 53297Epoch: 2025-12-04T12:32Z
TLE epoch observation values (Epoch: 2025-12-04T12:32:25.302Z)
Latitude
-0.00003°
Longitude
4.9145°
Altitude
473.98 km
Speed
7.629 km/s
True Right ascension
17h 46m 23s
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
11:54:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.611 km
Perigee altitude
469.706 km
Semi-major axis
6,850.795 km
Eccentricity
0.00043
Inclination
44.9764°
RAAN
266.5977°
Arg. of periapsis
175.4691°
True anomaly
184.61932°
Mean anomaly
184.6233°
Eccentric anomaly
184.62131°
Mean motion
3.82765 °/min
Orbital period
94.05 mins
BSTAR
0.0011553
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Other satellites on launch #247 in the year 2024 (2024-12-21 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-05 21:35:32.599Z | 190.674° SSW | 2025-12-05 21:37:32.599Z | 153.825° SSE | 20.823° | 2025-12-05 21:40:32.599Z | 93.035° ESE |
| 5 mins | 2025-12-05 23:14:32.599Z | 257.684° W | 2025-12-05 23:16:32.599Z | 26.444° NE | 42.919° | 2025-12-05 23:19:32.599Z | 64.183° ENE |
| 4 mins | 2025-12-06 00:53:32.599Z | 308.553° NW | 2025-12-06 00:55:32.599Z | 16.061° NNE | 29.642° | 2025-12-06 00:57:32.599Z | 58.226° ENE |
| 6 mins | 2025-12-06 02:31:32.599Z | 303.886° NW | 2025-12-06 02:33:32.599Z | 347.286° N | 36.26° | 2025-12-06 02:37:32.599Z | 92.459° ESE |
| 5 mins | 2025-12-06 04:10:32.599Z | 270.992° WNW | 2025-12-06 04:12:32.599Z | 209.051° SW | 33.474° | 2025-12-06 04:15:32.599Z | 142.962° 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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