KUIPER-00409, 68925
Orbit data source: Space-Track
KUIPER-00409, 68925 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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68925 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: 3 days ago
TLE from 3 days ago
0 KUIPER-00409
1 68925U 26098G 26155.09219770 .00027973 00000-0 85725-3 0 9997
2 68925 51.8722 130.9775 0008101 98.3496 261.8408 15.33547578 5336Epoch: 2026-06-04T02:12Z
TLE epoch observation values (Epoch: 2026-06-04T02:12:45.881Z)
Latitude
0°
Longitude
-154.7551°
Altitude
466.791 km
Speed
7.634 km/s
True Right ascension
08h 43m 54s
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
02:56:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.249 km
Perigee altitude
460.16 km
Semi-major axis
6,843.841 km
Eccentricity
0.00081
Inclination
51.8722°
RAAN
130.9775°
Arg. of periapsis
98.3496°
True anomaly
261.74892°
Mean anomaly
261.8408°
Eccentric anomaly
261.79486°
Mean motion
3.83348 °/min
Orbital period
93.91 mins
BSTAR
0.00085725
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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-00409 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 23:10:41.341Z | 168.854° S | 2026-06-06 23:12:41.341Z | 134.327° SE | 15.716° | 2026-06-06 23:14:41.341Z | 96.579° ESE |
| 5 mins | 2026-06-07 00:48:41.341Z | 255.036° W | 2026-06-07 00:50:41.341Z | 352.974° N | 39.688° | 2026-06-07 00:53:41.341Z | 45.529° ENE |
| 4 mins | 2026-06-07 05:44:41.341Z | 342.144° N | 2026-06-07 05:46:41.341Z | 33.128° NE | 23.802° | 2026-06-07 05:48:41.341Z | 76.263° E |
| 5 mins | 2026-06-07 07:22:41.341Z | 283.913° WNW | 2026-06-07 07:24:41.341Z | 203.532° SW | 35.694° | 2026-06-07 07:27:41.341Z | 148.604° SSE |
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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