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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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: 12 hours ago
TLE from 12 hours ago
0 XCUBE-1
1 62400U 24247Z 26094.04217684 .00015298 00000-0 55126-3 0 9991
2 62400 44.9979 338.1188 0003601 144.9455 215.1666 15.28463123 71617Epoch: 2026-04-04T01:00Z
TLE epoch observation values (Epoch: 2026-04-04T01:00:44.078Z)
Latitude
-0.00003°
Longitude
130.56748°
Altitude
482.423 km
Speed
7.625 km/s
True Right ascension
22h 32m 28s
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
19:15:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.487 km
Perigee altitude
479.546 km
Semi-major axis
6,860.153 km
Eccentricity
0.00036
Inclination
44.9979°
RAAN
338.1188°
Arg. of periapsis
144.9455°
True anomaly
215.14284°
Mean anomaly
215.1666°
Eccentric anomaly
215.15472°
Mean motion
3.81982 °/min
Orbital period
94.25 mins
BSTAR
0.00055126
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-04 18:26:55.874Z | 171.836° S | 2026-04-04 18:28:55.874Z | 133.474° SE | 16.56° | 2026-04-04 18:30:55.874Z | 99.678° ESE |
| 5 mins | 2026-04-04 20:04:55.874Z | 243.861° WSW | 2026-04-04 20:06:55.874Z | 183.367° SSW | 44.966° | 2026-04-04 20:09:55.874Z | 66.91° ENE |
| 5 mins | 2026-04-04 21:43:55.874Z | 296.269° NW | 2026-04-04 21:45:55.874Z | 353.579° N | 31.891° | 2026-04-04 21:48:55.874Z | 60.615° ENE |
| 5 mins | 2026-04-04 23:22:55.874Z | 307.693° NW | 2026-04-04 23:24:55.874Z | 2.729° NNE | 35.022° | 2026-04-04 23:27:55.874Z | 82.237° E |
| 5 mins | 2026-04-05 01:01:55.874Z | 278.863° WNW | 2026-04-05 01:03:55.874Z | 208.068° SW | 39.493° | 2026-04-05 01:06:55.874Z | 133.44° SE |
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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