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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XCUBE-1 radio frequencies
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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, 0.6 m
Radar Cross Section
0.138 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 XCUBE-1
1 62400U 24247Z 25260.26840528 .00006379 00000-0 27084-3 0 9990
2 62400 44.9933 341.1356 0003522 13.0715 347.0257 15.23888974 41242Epoch: 2025-09-17T06:26Z
TLE epoch observation values (Epoch: 2025-09-17T06:26:30.216Z)
Latitude
-0.00002°
Longitude
-111.93711°
Altitude
491.763 km
Speed
7.622 km/s
True Right ascension
22h 44m 32s
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
21:57:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.152 km
Perigee altitude
493.31 km
Semi-major axis
6,873.868 km
Eccentricity
0.00035
Inclination
44.9933°
RAAN
341.1356°
Arg. of periapsis
13.0715°
True anomaly
347.01663°
Mean anomaly
347.0257°
Eccentric anomaly
347.02117°
Mean motion
3.80839 °/min
Orbital period
94.53 mins
BSTAR
0.00027084
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 07:47:52.628Z | 185.686° SSW | 2025-09-18 07:49:52.628Z | 146.553° SSE | 20.967° | 2025-09-18 07:52:52.628Z | 91.152° ESE |
| 5 mins | 2025-09-18 09:26:52.628Z | 254.668° W | 2025-09-18 09:28:52.628Z | 354.691° N | 44.311° | 2025-09-18 09:31:52.628Z | 64.095° ENE |
| 5 mins | 2025-09-18 11:05:52.628Z | 296.885° NW | 2025-09-18 11:07:52.628Z | 344.804° N | 31.122° | 2025-09-18 11:10:52.628Z | 59.973° ENE |
| 5 mins | 2025-09-18 12:45:52.628Z | 311.393° NW | 2025-09-18 12:47:52.628Z | 30.602° NE | 37.518° | 2025-09-18 12:50:52.628Z | 90.393° ESE |
| 5 mins | 2025-09-18 14:24:52.628Z | 269.22° W | 2025-09-18 14:26:52.628Z | 200.797° SSW | 34.407° | 2025-09-18 14:29:52.628Z | 141.436° 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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