KUIPER-00016, 63732
Orbit data source: Space-Track
KUIPER-00016, 63732 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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63732 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00016
1 63732U 25088J 25348.41988293 -.00000844 00000-0 -81176-4 0 9995
2 63732 51.9023 128.6582 0013713 141.4526 218.7418 14.79909847 34706Epoch: 2025-12-14T10:04Z
TLE epoch observation values (Epoch: 2025-12-14T10:04:37.885Z)
Latitude
-0.00001°
Longitude
-105.83273°
Altitude
637.856 km
Speed
7.536 km/s
True Right ascension
08h 34m 37s
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
13:22:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.67 km
Perigee altitude
620.449 km
Semi-major axis
7,008.197 km
Eccentricity
0.00137
Inclination
51.9023°
RAAN
128.6582°
Arg. of periapsis
141.4526°
True anomaly
218.64359°
Mean anomaly
218.7418°
Eccentric anomaly
218.69268°
Mean motion
3.69942 °/min
Orbital period
97.31 mins
BSTAR
-0.000081176
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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-00016 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 15:37:12.991Z | 325.728° NNW | 2025-12-15 15:39:12.991Z | 355.103° N | 16.906° | 2025-12-15 15:42:12.991Z | 39.714° NE |
| 5 mins | 2025-12-15 17:20:12.991Z | 341.313° N | 2025-12-15 17:22:12.991Z | 22.991° NE | 25.815° | 2025-12-15 17:25:12.991Z | 75.966° E |
| 7 mins | 2025-12-15 19:01:12.991Z | 300.126° NW | 2025-12-15 19:04:12.991Z | 195.993° SSW | 42.907° | 2025-12-15 19:08:12.991Z | 138.222° SSE |
| 5 mins | 2025-12-16 10:52:12.991Z | 170.397° S | 2025-12-16 10:54:12.991Z | 130.18° SE | 25.109° | 2025-12-16 10:57:12.991Z | 79.368° E |
| 7 mins | 2025-12-16 12:32:12.991Z | 255.381° W | 2025-12-16 12:35:12.991Z | 315.751° NNW | 38.35° | 2025-12-16 12:39:12.991Z | 42.926° NE |
| 4 mins | 2025-12-16 14:16:12.991Z | 321.718° NNW | 2025-12-16 14:17:12.991Z | 338.616° N | 19.009° | 2025-12-16 14:20:12.991Z | 27.533° 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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