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 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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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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 KUIPER-00432
1 68937U 26098U 26126.25002315 .00055617 00000-0 16759-2 0 9997
2 68937 51.8753 269.8076 0011441 357.4766 65.5515 15.33725922 1783Epoch: 2026-05-06T06:00Z
TLE epoch observation values (Epoch: 2026-05-06T06:00:02.000Z)
Latitude
44.71874°
Longitude
6.29432°
Altitude
465.956 km
Speed
7.641 km/s
True Right ascension
21h 21m 39s
True Declination
44° 32' 22"
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
19:38:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.003 km
Perigee altitude
457.344 km
Semi-major axis
6,843.31 km
Eccentricity
0.00114
Inclination
51.8753°
RAAN
269.8076°
Arg. of periapsis
357.4766°
True anomaly
65.67092°
Mean anomaly
65.5515°
Eccentric anomaly
65.6112°
Mean motion
3.83393 °/min
Orbital period
93.9 mins
BSTAR
0.0016759
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-06 12:09:04.991Z | 209.122° SW | 2026-05-06 12:12:04.991Z | 133.311° SE | 36.215° | 2026-05-06 12:15:04.991Z | 64.377° ENE |
| 4 mins | 2026-05-06 13:48:04.991Z | 289.06° WNW | 2026-05-06 13:50:04.991Z | 338.714° N | 24.138° | 2026-05-06 13:52:04.991Z | 23.775° NE |
| 5 mins | 2026-05-06 18:44:04.991Z | 322.187° NNW | 2026-05-06 18:46:04.991Z | 39.387° NE | 40.593° | 2026-05-06 18:49:04.991Z | 113.606° SE |
| 5 mins | 2026-05-07 11:37:04.991Z | 191.438° SSW | 2026-05-07 11:39:04.991Z | 132.25° SE | 31.138° | 2026-05-07 11:42:04.991Z | 68.49° E |
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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