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
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 KUIPER-00432
1 68937U 26098U 26155.12303560 .00022902 00000-0 76254-3 0 9999
2 68937 51.8756 131.1800 0012133 95.7387 264.4981 15.30967892 5335Epoch: 2026-06-04T02:57Z
TLE epoch observation values (Epoch: 2026-06-04T02:57:10.275Z)
Latitude
-0.00002°
Longitude
-165.68465°
Altitude
474.491 km
Speed
7.629 km/s
True Right ascension
08h 44m 43s
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
14:07:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.701 km
Perigee altitude
465.076 km
Semi-major axis
6,851.526 km
Eccentricity
0.00121
Inclination
51.8756°
RAAN
131.18°
Arg. of periapsis
95.7387°
True anomaly
264.35973°
Mean anomaly
264.4981°
Eccentric anomaly
264.42891°
Mean motion
3.82703 °/min
Orbital period
94.07 mins
BSTAR
0.00076254
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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 | 2026-06-10 05:06:13.162Z | 321.922° NNW | 2026-06-10 05:09:13.162Z | 32.7° NE | 33.108° | 2026-06-10 05:12:13.162Z | 100.679° ESE |
| 4 mins | 2026-06-10 06:45:13.162Z | 269.294° W | 2026-06-10 06:47:13.162Z | 220.771° SW | 22.853° | 2026-06-10 06:49:13.162Z | 178.917° S |
| 4 mins | 2026-06-10 22:02:13.162Z | 176.689° S | 2026-06-10 22:04:13.162Z | 129.339° SE | 23.439° | 2026-06-10 22:06:13.162Z | 85.407° E |
| 5 mins | 2026-06-10 23:40:13.162Z | 273.74° WNW | 2026-06-10 23:42:13.162Z | 343.263° N | 32.474° | 2026-06-10 23:45:13.162Z | 40.027° 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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