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: 14 hours ago
TLE from 14 hours ago
0 XCUBE-1
1 62400U 24247Z 25316.29013158 .00022413 00000-0 88183-3 0 9990
2 62400 44.9984 36.6524 0006370 345.0649 15.0044 15.25310756 49793Epoch: 2025-11-12T06:57Z
TLE epoch observation values (Epoch: 2025-11-12T06:57:47.368Z)
Latitude
-0.00003°
Longitude
-119.45946°
Altitude
485.626 km
Speed
7.626 km/s
True Right ascension
02h 26m 36s
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
17:08:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.836 km
Perigee altitude
487.084 km
Semi-major axis
6,869.597 km
Eccentricity
0.00064
Inclination
44.9984°
RAAN
36.6524°
Arg. of periapsis
345.0649°
True anomaly
15.02331°
Mean anomaly
15.0044°
Eccentric anomaly
15.01385°
Mean motion
3.81194 °/min
Orbital period
94.44 mins
BSTAR
0.00088183
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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 | 2025-11-13 08:18:06.984Z | 211.244° SW | 2025-11-13 08:21:06.984Z | 146.759° SSE | 30.781° | 2025-11-13 08:24:06.984Z | 81.943° E |
| 5 mins | 2025-11-13 09:58:06.984Z | 274.504° WNW | 2025-11-13 10:00:06.984Z | 353.68° N | 39.519° | 2025-11-13 10:03:06.984Z | 60.601° ENE |
| 5 mins | 2025-11-13 11:37:06.984Z | 303.733° NW | 2025-11-13 11:39:06.984Z | 353.125° N | 30.826° | 2025-11-13 11:42:06.984Z | 65.685° ENE |
| 6 mins | 2025-11-13 13:16:06.984Z | 299.522° NW | 2025-11-13 13:19:06.984Z | 68.692° E | 40.734° | 2025-11-13 13:22:06.984Z | 103.763° ESE |
| 4 mins | 2025-11-13 14:56:06.984Z | 248.581° W | 2025-11-13 14:57:06.984Z | 223.309° SW | 24.26° | 2025-11-13 15:00:06.984Z | 161.779° 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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