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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00008
1 63724U 25088A 26090.97624219 .00002268 00000-0 35340-3 0 9998
2 63724 51.9022 348.9974 0001795 160.7046 199.3983 14.76454936 51358Epoch: 2026-03-31T23:25Z
TLE epoch observation values (Epoch: 2026-03-31T23:25:47.325Z)
Latitude
-0.00002°
Longitude
168.20449°
Altitude
642.471 km
Speed
7.537 km/s
True Right ascension
23h 15m 59s
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
14:26:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.247 km
Perigee altitude
639.727 km
Semi-major axis
7,019.124 km
Eccentricity
0.00018
Inclination
51.9022°
RAAN
348.9974°
Arg. of periapsis
160.7046°
True anomaly
199.39147°
Mean anomaly
199.3983°
Eccentric anomaly
199.39488°
Mean motion
3.69079 °/min
Orbital period
97.54 mins
BSTAR
0.0003534
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-01 19:04:06.227Z | 195.618° SSW | 2026-04-01 19:08:06.227Z | 130.805° SE | 29.126° | 2026-04-01 19:12:06.227Z | 68.993° E |
| 7 mins | 2026-04-01 20:47:06.227Z | 267.061° W | 2026-04-01 20:50:06.227Z | 347.903° N | 35.17° | 2026-04-01 20:54:06.227Z | 43.942° NE |
| 5 mins | 2026-04-01 22:30:06.227Z | 315.587° NNW | 2026-04-01 22:32:06.227Z | 347.086° N | 18.876° | 2026-04-01 22:35:06.227Z | 32.392° NE |
| 5 mins | 2026-04-02 00:13:06.227Z | 336.044° NNW | 2026-04-02 00:15:06.227Z | 8.202° NNE | 19.761° | 2026-04-02 00:18:06.227Z | 55.098° ENE |
| 7 mins | 2026-04-02 01:55:06.227Z | 322.347° NNW | 2026-04-02 01:58:06.227Z | 46.951° ENE | 38.899° | 2026-04-02 02:02:06.227Z | 110.029° ESE |
| 6 mins | 2026-04-02 03:37:06.227Z | 271.133° WNW | 2026-04-02 03:39:06.227Z | 234.448° WSW | 24.526° | 2026-04-02 03:43:06.227Z | 172.378° S |
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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