KUIPER-00014, 63730
Orbit data source: Space-Track
KUIPER-00014, 63730 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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63730 intel report (Beta)
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Edit Public Description
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: 21 hours ago
TLE from 21 hours ago
0 KUIPER-00014
1 63730U 25088G 25348.75999879 .00001819 00000-0 26734-3 0 9991
2 63730 51.9020 124.6125 0009744 162.9322 197.1969 14.79984087 34790Epoch: 2025-12-14T18:14Z
TLE epoch observation values (Epoch: 2025-12-14T18:14:23.895Z)
Latitude
-0.00009°
Longitude
127.34457°
Altitude
636.645 km
Speed
7.538 km/s
True Right ascension
08h 18m 26s
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
13:23:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.654 km
Perigee altitude
622.997 km
Semi-major axis
7,007.962 km
Eccentricity
0.00097
Inclination
51.902°
RAAN
124.6125°
Arg. of periapsis
162.9322°
True anomaly
197.16393°
Mean anomaly
197.1969°
Eccentric anomaly
197.18041°
Mean motion
3.69961 °/min
Orbital period
97.31 mins
BSTAR
0.00026734
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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-00014 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-15 15:41:16.805Z | 326.24° NNW | 2025-12-15 15:44:16.805Z | 11.773° NNE | 17.124° | 2025-12-15 15:46:16.805Z | 40.758° NE |
| 7 mins | 2025-12-15 17:23:16.805Z | 327.266° NNW | 2025-12-15 17:26:16.805Z | 22.398° NNE | 28.785° | 2025-12-15 17:30:16.805Z | 89.14° E |
| 7 mins | 2025-12-15 19:05:16.805Z | 292.827° NW | 2025-12-15 19:08:16.805Z | 208.574° SW | 38.769° | 2025-12-15 19:12:16.805Z | 146.728° SSE |
| 6 mins | 2025-12-16 10:55:16.805Z | 189.702° SSW | 2025-12-16 10:58:16.805Z | 127.303° SE | 30.316° | 2025-12-16 11:01:16.805Z | 73.482° E |
| 7 mins | 2025-12-16 12:36:16.805Z | 263.842° W | 2025-12-16 12:39:16.805Z | 321.87° NNW | 34.544° | 2025-12-16 12:43:16.805Z | 40.454° NE |
| 4 mins | 2025-12-16 14:20:16.805Z | 324.171° NNW | 2025-12-16 14:22:16.805Z | 357.956° N | 18.205° | 2025-12-16 14:24:16.805Z | 28.12° NE |
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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