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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 XCUBE-1
1 62400U 24247Z 26130.37356080 .00004839 00000-0 17890-3 0 9997
2 62400 44.9943 139.4179 0004605 340.6380 19.4328 15.29015025 77179Epoch: 2026-05-10T08:57Z
TLE epoch observation values (Epoch: 2026-05-10T08:57:55.653Z)
Latitude
0°
Longitude
136.75844°
Altitude
475.776 km
Speed
7.631 km/s
True Right ascension
09h 17m 40s
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
13:50:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.525 km
Perigee altitude
477.208 km
Semi-major axis
6,858.504 km
Eccentricity
0.00046
Inclination
44.9943°
RAAN
139.4179°
Arg. of periapsis
340.638°
True anomaly
19.45037°
Mean anomaly
19.4328°
Eccentric anomaly
19.44158°
Mean motion
3.82119 °/min
Orbital period
94.21 mins
BSTAR
0.0001789
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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 | 2026-05-12 06:48:12.976Z | 297.621° NW | 2026-05-12 06:51:12.976Z | 355.198° N | 31.581° | 2026-05-12 06:54:12.976Z | 71.723° E |
| 5 mins | 2026-05-12 08:28:12.976Z | 292.803° NW | 2026-05-12 08:30:12.976Z | 279.861° WNW | 44.499° | 2026-05-12 08:33:12.976Z | 116.022° SE |
| 5 mins | 2026-05-13 03:02:12.976Z | 220.578° SW | 2026-05-13 03:04:12.976Z | 173.197° S | 37.42° | 2026-05-13 03:07:12.976Z | 77.498° E |
| 5 mins | 2026-05-13 04:41:12.976Z | 282.706° WNW | 2026-05-13 04:43:12.976Z | 341.532° N | 35.651° | 2026-05-13 04:46:12.976Z | 58.438° ENE |
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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