KUIPER-00432, 68937
Orbit data source: Space-Track
KUIPER-00432, 68937 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 30 Apr 2026 UTC via an ARIANE 64 launch vehicle from the French Guiana (FRGUI). 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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68937 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 3.4 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00432
1 68937U 26098U 26171.38844479 .00004963 00000-0 18560-3 0 9997
2 68937 51.8768 53.4228 0013443 160.2782 199.8724 15.29041819 7822Epoch: 2026-06-20T09:19Z
TLE epoch observation values (Epoch: 2026-06-20T09:19:21.629Z)
Latitude
-0.00001°
Longitude
4.97889°
Altitude
488.106 km
Speed
7.618 km/s
True Right ascension
03h 33m 41s
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
07:21:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.358 km
Perigee altitude
469.922 km
Semi-major axis
6,857.277 km
Eccentricity
0.00134
Inclination
51.8768°
RAAN
53.4228°
Arg. of periapsis
160.2782°
True anomaly
199.82012°
Mean anomaly
199.8724°
Eccentric anomaly
199.84625°
Mean motion
3.82222 °/min
Orbital period
94.19 mins
BSTAR
0.0001856
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Other satellites on launch #98 in the year 2026 (2026-04-30 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-00432 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 | 2026-06-20 20:33:48.326Z | 289.862° WNW | 2026-06-20 20:35:48.326Z | 330.159° NNW | 21.89° | 2026-06-20 20:38:48.326Z | 29.661° NE |
| 4 mins | 2026-06-20 23:52:48.326Z | 345.711° N | 2026-06-20 23:54:48.326Z | 26.755° NE | 17.578° | 2026-06-20 23:56:48.326Z | 61.813° ENE |
| 5 mins | 2026-06-21 01:30:48.326Z | 312.545° NW | 2026-06-21 01:32:48.326Z | 356.067° N | 43.887° | 2026-06-21 01:35:48.326Z | 122.825° SE |
| 6 mins | 2026-06-21 18:26:48.326Z | 211.161° SW | 2026-06-21 18:28:48.326Z | 167.582° S | 38.338° | 2026-06-21 18:32:48.326Z | 59.844° ENE |
| 4 mins | 2026-06-21 20:05:48.326Z | 295.001° NW | 2026-06-21 20:07:48.326Z | 343.731° N | 23.076° | 2026-06-21 20:09:48.326Z | 24.724° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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