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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 XCUBE-1
1 62400U 24247Z 26311.12842527 .00008888 00000-0 29599-3 0 9994
2 62400 44.9949 228.5088 0002385 306.1635 53.9029 15.31521107104861Epoch: 2026-11-07T03:04Z
TLE epoch observation values (Epoch: 2026-11-07T03:04:55.943Z)
Latitude
0.00001°
Longitude
135.93759°
Altitude
470.309 km
Speed
7.633 km/s
True Right ascension
15h 14m 02s
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
02:40:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.52 km
Perigee altitude
471.252 km
Semi-major axis
6,851.023 km
Eccentricity
0.00024
Inclination
44.9949°
RAAN
228.5088°
Arg. of periapsis
306.1635°
True anomaly
53.92499°
Mean anomaly
53.9029°
Eccentric anomaly
53.91394°
Mean motion
3.82745 °/min
Orbital period
94.06 mins
BSTAR
0.00029599
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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 | 2026-11-08 21:33:01.669Z | 227.691° WSW | 2026-11-08 21:36:01.669Z | 172.553° S | 53.463° | 2026-11-08 21:39:01.669Z | 75.836° E |
| 5 mins | 2026-11-08 23:13:01.669Z | 286.753° WNW | 2026-11-08 23:15:01.669Z | 352.934° N | 44.289° | 2026-11-08 23:18:01.669Z | 59.295° ENE |
| 5 mins | 2026-11-09 00:52:01.669Z | 311.368° NW | 2026-11-09 00:54:01.669Z | 11.409° NNE | 37.621° | 2026-11-09 00:57:01.669Z | 73.946° E |
| 6 mins | 2026-11-09 02:30:01.669Z | 293.817° NW | 2026-11-09 02:33:01.669Z | 114.6° SE | 72.652° | 2026-11-09 02:36:01.669Z | 114.837° SE |
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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