XCUBE-1, 62400
Orbit data source: Space-Track
XCUBE-1, 62400 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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62400 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
EXOBOT
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.138 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 XCUBE-1
1 62400U 24247Z 25312.03296855 .00013800 00000-0 55011-3 0 9999
2 62400 44.9970 59.8107 0006801 321.4811 38.5586 15.25178016 49141Epoch: 2025-11-08T00:47Z
TLE epoch observation values (Epoch: 2025-11-08T00:47:28.482Z)
Latitude
0.00003°
Longitude
0.47366°
Altitude
486.598 km
Speed
7.626 km/s
True Right ascension
03h 59m 14s
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
21:29:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.531 km
Perigee altitude
487.187 km
Semi-major axis
6,869.996 km
Eccentricity
0.00068
Inclination
44.997°
RAAN
59.8107°
Arg. of periapsis
321.4811°
True anomaly
38.60721°
Mean anomaly
38.5586°
Eccentric anomaly
38.5829°
Mean motion
3.81161 °/min
Orbital period
94.45 mins
BSTAR
0.00055011
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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.XCUBE-1 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 | 2025-11-09 09:59:05.813Z | 214.32° SW | 2025-11-09 10:02:05.813Z | 164.154° S | 30.109° | 2025-11-09 10:05:05.813Z | 85.485° E |
| 6 mins | 2025-11-09 11:39:05.813Z | 270.661° WNW | 2025-11-09 11:41:05.813Z | 320.296° NNW | 38.842° | 2025-11-09 11:45:05.813Z | 62.635° ENE |
| 5 mins | 2025-11-09 13:19:05.813Z | 311.469° NW | 2025-11-09 13:21:05.813Z | 14.669° NNE | 30.671° | 2025-11-09 13:24:05.813Z | 69.762° E |
| 5 mins | 2025-11-09 14:58:05.813Z | 302.007° NW | 2025-11-09 15:00:05.813Z | 22.03° NNE | 43.064° | 2025-11-09 15:03:05.813Z | 102.785° ESE |
| 4 mins | 2025-11-09 16:37:05.813Z | 257.475° W | 2025-11-09 16:39:05.813Z | 208.555° SW | 24.125° | 2025-11-09 16:41:05.813Z | 167.46° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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