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: 13 hours ago
TLE from 13 hours ago
0 XCUBE-1
1 62400U 24247Z 26036.70151795 .00015648 00000-0 58407-3 0 9994
2 62400 44.9971 291.2905 0004952 163.0939 197.0109 15.27283902 62843Epoch: 2026-02-05T16:50Z
TLE epoch observation values (Epoch: 2026-02-05T16:50:11.150Z)
Latitude
-0.00008°
Longitude
-97.10601°
Altitude
487.183 km
Speed
7.621 km/s
True Right ascension
19h 25m 09s
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
08:23:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.944 km
Perigee altitude
482.146 km
Semi-major axis
6,863.682 km
Eccentricity
0.0005
Inclination
44.9971°
RAAN
291.2905°
Arg. of periapsis
163.0939°
True anomaly
196.99431°
Mean anomaly
197.0109°
Eccentric anomaly
197.0026°
Mean motion
3.81687 °/min
Orbital period
94.32 mins
BSTAR
0.00058407
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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 | 2026-02-06 19:42:53.377Z | 214.438° SW | 2026-02-06 19:45:53.377Z | 150.381° SSE | 32.373° | 2026-02-06 19:48:53.377Z | 81.074° E |
| 5 mins | 2026-02-06 21:22:53.377Z | 277.435° WNW | 2026-02-06 21:24:53.377Z | 356.068° N | 38.533° | 2026-02-06 21:27:53.377Z | 60.492° ENE |
| 5 mins | 2026-02-06 23:01:53.377Z | 306.365° NW | 2026-02-06 23:03:53.377Z | 0.349° NNE | 30.895° | 2026-02-06 23:06:53.377Z | 68.026° E |
| 5 mins | 2026-02-07 00:40:53.377Z | 299.74° NW | 2026-02-07 00:42:53.377Z | 352.111° N | 43.148° | 2026-02-07 00:45:53.377Z | 104.223° ESE |
| 4 mins | 2026-02-07 02:19:53.377Z | 257.094° W | 2026-02-07 02:21:53.377Z | 210.371° SW | 22.51° | 2026-02-07 02:23:53.377Z | 169.87° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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