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 25346.73607287 .00012170 00000-0 47371-3 0 9997
2 62400 45.0000 230.9231 0006555 184.1510 175.9319 15.26076023 54448Epoch: 2025-12-12T17:39Z
TLE epoch observation values (Epoch: 2025-12-12T17:39:56.695Z)
Latitude
-0.00004°
Longitude
-115.73659°
Altitude
492.044 km
Speed
7.618 km/s
True Right ascension
15h 23m 41s
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
05:22:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.666 km
Perigee altitude
484.663 km
Semi-major axis
6,867.301 km
Eccentricity
0.00066
Inclination
45°
RAAN
230.9231°
Arg. of periapsis
184.151°
True anomaly
175.93722°
Mean anomaly
175.9319°
Eccentric anomaly
175.93456°
Mean motion
3.81385 °/min
Orbital period
94.39 mins
BSTAR
0.00047371
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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 | 2025-12-13 18:59:09.999Z | 199.324° SSW | 2025-12-13 19:02:09.999Z | 135.328° SSE | 25.024° | 2025-12-13 19:04:09.999Z | 93.504° ESE |
| 6 mins | 2025-12-13 20:38:09.999Z | 261.153° W | 2025-12-13 20:40:09.999Z | 299.819° NW | 40.943° | 2025-12-13 20:44:09.999Z | 63.38° ENE |
| 5 mins | 2025-12-13 22:18:09.999Z | 308.638° NW | 2025-12-13 22:20:09.999Z | 12.059° NNE | 30.418° | 2025-12-13 22:23:09.999Z | 66.639° ENE |
| 5 mins | 2025-12-13 23:57:09.999Z | 306.577° NW | 2025-12-13 23:59:09.999Z | 20.567° NNE | 40.099° | 2025-12-14 00:02:09.999Z | 94.946° ESE |
| 5 mins | 2025-12-14 01:36:09.999Z | 263.451° W | 2025-12-14 01:38:09.999Z | 204.284° SW | 29.509° | 2025-12-14 01:41:09.999Z | 148.512° SSE |
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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