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.
Embed this page
62400 intel report (Beta)
XCUBE-1 radio frequencies
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 XCUBE-1
1 62400U 24247Z 25241.25609691 .00008470 00000-0 35935-3 0 9990
2 62400 44.9965 84.3233 0004374 272.9502 87.0879 15.23541505 38347
TLE epoch observation values (Epoch: 2025-08-29T06:08:46.773Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #247 in the year 2024 (2024-12-21 UTC)
XCUBE-1 Visibility forecast
Observer location: undefined°, undefined°
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 | 2025-08-30 16:59:38.250Z | 237.157° WSW | 2025-08-30 17:02:38.250Z | 110.545° ESE | 43.314° | 2025-08-30 17:05:38.250Z | 69.2° E |
5 mins | 2025-08-30 18:39:38.250Z | 293.04° NW | 2025-08-30 18:41:38.250Z | 352.195° N | 33.421° | 2025-08-30 18:44:38.250Z | 59.752° ENE |
6 mins | 2025-08-30 20:18:38.250Z | 304.613° NW | 2025-08-30 20:21:38.250Z | 32.865° NE | 33.114° | 2025-08-30 20:24:38.250Z | 82.535° E |
6 mins | 2025-08-30 21:57:38.250Z | 287.197° WNW | 2025-08-30 22:00:38.250Z | 178.356° S | 41.785° | 2025-08-30 22:03:38.250Z | 126.721° 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 ascending order |
---|
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
---|
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|