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 shape, 3.4 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00409
1 68925U 26098G 26171.39268206 .00017115 00000-0 55799-3 0 9991
2 68925 51.8768 52.7218 0006697 165.3994 194.7185 15.31888815 7838Epoch: 2026-06-20T09:25Z
TLE epoch observation values (Epoch: 2026-06-20T09:25:27.729Z)
Latitude
-0.00005°
Longitude
2.74827°
Altitude
475.375 km
Speed
7.627 km/s
True Right ascension
03h 30m 53s
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
08:41:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.229 km
Perigee altitude
466.056 km
Semi-major axis
6,848.779 km
Eccentricity
0.00067
Inclination
51.8768°
RAAN
52.7218°
Arg. of periapsis
165.3994°
True anomaly
194.69902°
Mean anomaly
194.7185°
Eccentric anomaly
194.70876°
Mean motion
3.82934 °/min
Orbital period
94.01 mins
BSTAR
0.00055799
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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 | 2026-06-20 23:57:55.890Z | 351.009° N | 2026-06-20 23:58:55.890Z | 12.103° NNE | 18.51° | 2026-06-21 00:01:55.890Z | 68.248° E |
| 5 mins | 2026-06-21 01:35:55.890Z | 308.054° NW | 2026-06-21 01:37:55.890Z | 127.952° SE | 43.502° | 2026-06-21 01:40:55.890Z | 128.737° SE |
| 6 mins | 2026-06-21 18:28:55.890Z | 217.944° SW | 2026-06-21 18:31:55.890Z | 124.01° SE | 41.499° | 2026-06-21 18:34:55.890Z | 59.09° ENE |
| 4 mins | 2026-06-21 20:08:55.890Z | 310.93° NW | 2026-06-21 20:09:55.890Z | 336.212° NNW | 21.842° | 2026-06-21 20:12:55.890Z | 32.048° 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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