KUIPER-00008, 63724
Orbit data source: Space-Track
KUIPER-00008, 63724 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 28 Apr 2025 UTC via an ATLAS V 551 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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63724 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 KUIPER-00008
1 63724U 25088A 26154.97160698 .00000863 00000-0 14203-3 0 9999
2 63724 51.9007 66.4692 0001026 109.2926 250.8148 14.79982538 60827Epoch: 2026-06-03T23:19Z
TLE epoch observation values (Epoch: 2026-06-03T23:19:06.843Z)
Latitude
0.00005°
Longitude
-175.73184°
Altitude
630.362 km
Speed
7.544 km/s
True Right ascension
04h 25m 52s
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
13:52:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.549 km
Perigee altitude
629.111 km
Semi-major axis
7,007.967 km
Eccentricity
0.0001
Inclination
51.9007°
RAAN
66.4692°
Arg. of periapsis
109.2926°
True anomaly
250.8037°
Mean anomaly
250.8148°
Eccentric anomaly
250.80925°
Mean motion
3.6996 °/min
Orbital period
97.31 mins
BSTAR
0.00014203
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Other satellites on launch #88 in the year 2025 (2025-04-28 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.KUIPER-00008 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 | 2026-06-07 04:03:02.055Z | 278.047° WNW | 2026-06-07 04:06:02.055Z | 234.853° WSW | 19.85° | 2026-06-07 04:09:02.055Z | 187.876° SSW |
| 7 mins | 2026-06-07 19:53:02.055Z | 230.953° WSW | 2026-06-07 19:56:02.055Z | 230.618° WSW | 43.864° | 2026-06-07 20:00:02.055Z | 52.315° ENE |
| 6 mins | 2026-06-07 21:36:02.055Z | 297.717° NW | 2026-06-07 21:38:02.055Z | 332.711° NNW | 23.273° | 2026-06-07 21:42:02.055Z | 36.312° NE |
| 5 mins | 2026-06-07 23:19:02.055Z | 330.514° NNW | 2026-06-07 23:21:02.055Z | 1.258° NNE | 17.218° | 2026-06-07 23:24:02.055Z | 44.085° NE |
| 6 mins | 2026-06-08 01:01:02.055Z | 332.204° NNW | 2026-06-08 01:04:02.055Z | 32.487° NE | 27.021° | 2026-06-08 01:07:02.055Z | 81.521° E |
| 7 mins | 2026-06-08 02:42:02.055Z | 299.395° NW | 2026-06-08 02:45:02.055Z | 249.985° W | 40.822° | 2026-06-08 02:49:02.055Z | 143.756° 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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