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: 6 hours ago
TLE from 6 hours ago
0 XCUBE-1
1 62400U 24247Z 26177.53303429 .00007265 00000-0 25754-3 0 9999
2 62400 44.9944 241.2570 0004733 277.5169 82.5177 15.29733514 84397Epoch: 2026-06-26T12:47Z
TLE epoch observation values (Epoch: 2026-06-26T12:47:34.162Z)
Latitude
-0.00003°
Longitude
134.70445°
Altitude
476.185 km
Speed
7.63 km/s
True Right ascension
16h 05m 01s
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
06:21:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.465 km
Perigee altitude
474.975 km
Semi-major axis
6,856.357 km
Eccentricity
0.00047
Inclination
44.9944°
RAAN
241.257°
Arg. of periapsis
277.5169°
True anomaly
82.57148°
Mean anomaly
82.5177°
Eccentric anomaly
82.54459°
Mean motion
3.82299 °/min
Orbital period
94.17 mins
BSTAR
0.00025754
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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 | 2026-06-27 07:49:39.311Z | 231.418° WSW | 2026-06-27 07:51:39.311Z | 191.321° SSW | 41.404° | 2026-06-27 07:55:39.311Z | 70.027° E |
| 5 mins | 2026-06-27 09:28:39.311Z | 288.123° WNW | 2026-06-27 09:30:39.311Z | 342.298° N | 33.546° | 2026-06-27 09:33:39.311Z | 58.206° ENE |
| 5 mins | 2026-06-27 11:07:39.311Z | 306.742° NW | 2026-06-27 11:09:39.311Z | 356.509° N | 32.6° | 2026-06-27 11:12:39.311Z | 75.201° E |
| 5 mins | 2026-06-27 12:46:39.311Z | 287.948° WNW | 2026-06-27 12:48:39.311Z | 224.543° SW | 43.83° | 2026-06-27 12:51:39.311Z | 122.783° 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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