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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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-00014
1 63730U 25088G 26155.11882914 -.00001899 00000-0 -22017-3 0 9999
2 63730 51.9027 85.8608 0000737 147.7758 212.3249 14.79941374 60183Epoch: 2026-06-04T02:51Z
TLE epoch observation values (Epoch: 2026-06-04T02:51:06.837Z)
Latitude
-0.00007°
Longitude
150.51458°
Altitude
630.693 km
Speed
7.544 km/s
True Right ascension
05h 43m 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
13:54:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.476 km
Perigee altitude
629.443 km
Semi-major axis
7,008.097 km
Eccentricity
0.00007
Inclination
51.9027°
RAAN
85.8608°
Arg. of periapsis
147.7758°
True anomaly
212.32038°
Mean anomaly
212.3249°
Eccentric anomaly
212.32264°
Mean motion
3.6995 °/min
Orbital period
97.31 mins
BSTAR
-0.00022017
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-07 04:17:22.173Z | 302.833° NW | 2026-06-07 04:21:22.173Z | 241.878° WSW | 42.492° | 2026-06-07 04:25:22.173Z | 140.508° SSE |
| 6 mins | 2026-06-07 20:09:22.173Z | 177.122° S | 2026-06-07 20:11:22.173Z | 140.394° SSE | 25.589° | 2026-06-07 20:15:22.173Z | 73.871° E |
| 7 mins | 2026-06-07 21:50:22.173Z | 260.681° W | 2026-06-07 21:53:22.173Z | 345.368° N | 37.446° | 2026-06-07 21:57:22.173Z | 44.748° NE |
| 5 mins | 2026-06-07 23:33:22.173Z | 315.995° NNW | 2026-06-07 23:35:22.173Z | 349.382° N | 19.212° | 2026-06-07 23:38:22.173Z | 33.696° NE |
| 5 mins | 2026-06-08 01:16:22.173Z | 341.308° N | 2026-06-08 01:18:22.173Z | 15.183° NNE | 18.758° | 2026-06-08 01:21:22.173Z | 57.242° ENE |
| 7 mins | 2026-06-08 02:57:22.173Z | 322.457° NNW | 2026-06-08 03:00:22.173Z | 27.198° NE | 36.541° | 2026-06-08 03:04:22.173Z | 103.938° ESE |
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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