KUIPER-00451, 68945
Orbit data source: Space-Track
KUIPER-00451, 68945 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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68945 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: 4 days ago
TLE from 4 days ago
0 KUIPER-00451
1 68945U 26098AC 26154.17447080 .00019587 00000-0 71111-3 0 9990
2 68945 51.8756 136.0778 0013807 98.1410 262.1140 15.28229692 5186Epoch: 2026-06-03T04:11Z
TLE epoch observation values (Epoch: 2026-06-03T04:11:14.277Z)
Latitude
0.00003°
Longitude
-178.36854°
Altitude
483.177 km
Speed
7.624 km/s
True Right ascension
09h 04m 18s
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
03:06:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.04 km
Perigee altitude
472.098 km
Semi-major axis
6,859.706 km
Eccentricity
0.00138
Inclination
51.8756°
RAAN
136.0778°
Arg. of periapsis
98.141°
True anomaly
261.95732°
Mean anomaly
262.114°
Eccentric anomaly
262.03565°
Mean motion
3.82019 °/min
Orbital period
94.24 mins
BSTAR
0.00071111
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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-00451 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-06 23:22:13.410Z | 172.278° S | 2026-06-06 23:24:13.410Z | 134.105° SE | 19.006° | 2026-06-06 23:26:13.410Z | 93.295° ESE |
| 5 mins | 2026-06-07 01:00:13.410Z | 259.397° W | 2026-06-07 01:02:13.410Z | 325.223° NNW | 37.773° | 2026-06-07 01:05:13.410Z | 41.361° NE |
| 5 mins | 2026-06-07 05:57:13.410Z | 333.997° NNW | 2026-06-07 05:59:13.410Z | 20.581° NNE | 26.836° | 2026-06-07 06:02:13.410Z | 87.433° E |
| 5 mins | 2026-06-07 07:35:13.410Z | 286.207° WNW | 2026-06-07 07:37:13.410Z | 241.068° WSW | 31.232° | 2026-06-07 07:40:13.410Z | 160.433° S |
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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