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: 20 hours ago
TLE from 20 hours ago
0 KUIPER-00014
1 63730U 25088G 26090.48570330 .00009253 00000-0 11379-2 0 9991
2 63730 51.9035 12.2829 0001435 173.0590 187.0394 14.83581718 50605Epoch: 2026-03-31T11:39Z
TLE epoch observation values (Epoch: 2026-03-31T11:39:24.765Z)
Latitude
-0.00001°
Longitude
8.5675°
Altitude
619.786 km
Speed
7.55 km/s
True Right ascension
00h 49m 07s
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
12:48:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.496 km
Perigee altitude
617.488 km
Semi-major axis
6,996.629 km
Eccentricity
0.00014
Inclination
51.9035°
RAAN
12.2829°
Arg. of periapsis
173.059°
True anomaly
187.03739°
Mean anomaly
187.0394°
Eccentric anomaly
187.03839°
Mean motion
3.7086 °/min
Orbital period
97.07 mins
BSTAR
0.0011379
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-01 20:08:06.676Z | 178.861° S | 2026-04-01 20:11:06.676Z | 133.71° SE | 21.306° | 2026-04-01 20:14:06.676Z | 84.322° E |
| 7 mins | 2026-04-01 21:49:06.676Z | 249.475° W | 2026-04-01 21:52:06.676Z | 318.872° NNW | 41.106° | 2026-04-01 21:56:06.676Z | 45.606° ENE |
| 5 mins | 2026-04-01 23:32:06.676Z | 311.074° NW | 2026-04-01 23:34:06.676Z | 345.408° N | 20.008° | 2026-04-01 23:37:06.676Z | 31.795° NE |
| 4 mins | 2026-04-02 01:15:06.676Z | 342.294° N | 2026-04-02 01:17:06.676Z | 15.965° NNE | 17.493° | 2026-04-02 01:19:06.676Z | 45.451° ENE |
| 6 mins | 2026-04-02 02:56:06.676Z | 328.372° NNW | 2026-04-02 02:59:06.676Z | 38.878° NE | 32.463° | 2026-04-02 03:02:06.676Z | 93.386° ESE |
| 7 mins | 2026-04-02 04:37:06.676Z | 286.795° WNW | 2026-04-02 04:40:06.676Z | 222.913° SW | 32.528° | 2026-04-02 04:44:06.676Z | 157.408° 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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