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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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: 5 days ago
TLE from 5 days ago
0 KUIPER-00016
1 63732U 25088J 26153.15781504 .00001925 00000-0 28149-3 0 9996
2 63732 51.8992 97.0500 0000903 98.9646 261.1418 14.79929445 59856Epoch: 2026-06-02T03:47Z
TLE epoch observation values (Epoch: 2026-06-02T03:47:15.219Z)
Latitude
-0.00006°
Longitude
149.60173°
Altitude
630.391 km
Speed
7.544 km/s
True Right ascension
06h 28m 11s
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
13:52:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.631 km
Perigee altitude
629.365 km
Semi-major axis
7,008.135 km
Eccentricity
0.00009
Inclination
51.8992°
RAAN
97.05°
Arg. of periapsis
98.9646°
True anomaly
261.13158°
Mean anomaly
261.1418°
Eccentric anomaly
261.13669°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00028149
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-07 04:12:36.391Z | 306.849° NW | 2026-06-07 04:17:36.391Z | 141.981° SSE | 43.632° | 2026-06-07 04:21:36.391Z | 130.862° SE |
| 5 mins | 2026-06-07 20:05:36.391Z | 161.015° S | 2026-06-07 20:07:36.391Z | 124.857° SE | 20.791° | 2026-06-07 20:10:36.391Z | 80.999° E |
| 7 mins | 2026-06-07 21:45:36.391Z | 248.822° W | 2026-06-07 21:48:36.391Z | 332.697° NNW | 41.768° | 2026-06-07 21:52:36.391Z | 46.613° ENE |
| 5 mins | 2026-06-07 23:28:36.391Z | 309.714° NW | 2026-06-07 23:30:36.391Z | 343.864° N | 20.523° | 2026-06-07 23:33:36.391Z | 30.986° NE |
| 5 mins | 2026-06-08 01:11:36.391Z | 337.529° N | 2026-06-08 01:13:36.391Z | 9.953° NNE | 17.944° | 2026-06-08 01:16:36.391Z | 52.065° ENE |
| 6 mins | 2026-06-08 02:53:36.391Z | 333.058° NNW | 2026-06-08 02:55:36.391Z | 17.622° NNE | 32.362° | 2026-06-08 02:59:36.391Z | 95.245° 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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