KUIPER-00431, 68936
Orbit data source: Space-Track
KUIPER-00431, 68936 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 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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68936 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 KUIPER-00431
1 68936U 26098T 26126.25002315 .00054327 00000-0 16868-2 0 9994
2 68936 51.8757 269.8525 0017294 5.3588 35.2309 15.32703380 1810Epoch: 2026-05-06T06:00Z
TLE epoch observation values (Epoch: 2026-05-06T06:00:02.000Z)
Latitude
30.96588°
Longitude
-16.34504°
Altitude
459.805 km
Speed
7.646 km/s
True Right ascension
19h 51m 06s
True Declination
30° 48' 28"
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
19:39:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.056 km
Perigee altitude
456.376 km
Semi-major axis
6,846.353 km
Eccentricity
0.00173
Inclination
51.8757°
RAAN
269.8525°
Arg. of periapsis
5.3588°
True anomaly
35.34542°
Mean anomaly
35.2309°
Eccentric anomaly
35.28814°
Mean motion
3.83137 °/min
Orbital period
93.96 mins
BSTAR
0.0016868
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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-00431 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 | 2026-05-06 12:14:53.666Z | 215.806° SW | 2026-05-06 12:17:53.666Z | 169.596° S | 37.403° | 2026-05-06 12:20:53.666Z | 64.25° ENE |
| 4 mins | 2026-05-06 13:54:53.666Z | 298.551° NW | 2026-05-06 13:55:53.666Z | 321.695° NNW | 22.1° | 2026-05-06 13:58:53.666Z | 27.621° NE |
| 5 mins | 2026-05-06 18:50:53.666Z | 319.644° NNW | 2026-05-06 18:52:53.666Z | 65.255° ENE | 42.066° | 2026-05-06 18:55:53.666Z | 118.642° SE |
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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