KUIPER-00414, 68929
Orbit data source: Space-Track
KUIPER-00414, 68929 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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68929 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-00414
1 68929U 26098L 26126.25002315 .00054033 00000-0 17483-2 0 9994
2 68929 51.8775 269.8860 0020761 6.3502 18.8363 15.31324492 1307Epoch: 2026-05-06T06:00Z
TLE epoch observation values (Epoch: 2026-05-06T06:00:02.000Z)
Latitude
19.66102°
Longitude
-28.04584°
Altitude
458.707 km
Speed
7.648 km/s
True Right ascension
19h 04m 18s
True Declination
19° 32' 51"
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
19:38:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.547 km
Perigee altitude
458.102 km
Semi-major axis
6,850.462 km
Eccentricity
0.00208
Inclination
51.8775°
RAAN
269.886°
Arg. of periapsis
6.3502°
True anomaly
18.9133°
Mean anomaly
18.8363°
Eccentric anomaly
18.87478°
Mean motion
3.82792 °/min
Orbital period
94.05 mins
BSTAR
0.0017483
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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-00414 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 12:19:53.633Z | 217.375° SW | 2026-05-06 12:22:53.633Z | 135.807° SSE | 41.069° | 2026-05-06 12:25:53.633Z | 59.977° ENE |
| 4 mins | 2026-05-06 13:59:53.633Z | 307.556° NW | 2026-05-06 14:00:53.633Z | 332.44° NNW | 21.81° | 2026-05-06 14:03:53.633Z | 30.926° NE |
| 6 mins | 2026-05-06 18:54:53.633Z | 312.565° NW | 2026-05-06 18:57:53.633Z | 85.661° E | 42.623° | 2026-05-06 19:00:53.633Z | 122.071° SE |
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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