KUIPER-00412, 68927
Orbit data source: Space-Track
KUIPER-00412, 68927 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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68927 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: 7 hours ago
TLE from 7 hours ago
0 KUIPER-00412
1 68927U 26098J 26126.25002315 .00056060 00000-0 15748-2 0 9996
2 68927 51.8778 269.7172 0002449 70.0833 38.2251 15.35984870 1927Epoch: 2026-05-06T06:00Z
TLE epoch observation values (Epoch: 2026-05-06T06:00:02.000Z)
Latitude
48.46399°
Longitude
73.8396°
Altitude
462.01 km
Speed
7.642 km/s
True Right ascension
01h 51m 50s
True Declination
48° 17' 09"
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
20:27:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.137 km
Perigee altitude
456.788 km
Semi-major axis
6,836.6 km
Eccentricity
0.00024
Inclination
51.8778°
RAAN
269.7172°
Arg. of periapsis
70.0833°
True anomaly
38.24247°
Mean anomaly
38.2251°
Eccentric anomaly
38.23378°
Mean motion
3.83957 °/min
Orbital period
93.76 mins
BSTAR
0.0015748
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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-00412 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-06 13:34:07.907Z | 270.708° WNW | 2026-05-06 13:37:07.907Z | 339.638° N | 27.255° | 2026-05-06 13:39:07.907Z | 26.987° NE |
| 4 mins | 2026-05-06 18:31:07.907Z | 336.33° NNW | 2026-05-06 18:32:07.907Z | 7.582° NNE | 33.992° | 2026-05-06 18:35:07.907Z | 101.538° ESE |
| 5 mins | 2026-05-07 11:22:07.907Z | 180.795° SSW | 2026-05-07 11:24:07.907Z | 132.974° SE | 24.388° | 2026-05-07 11:27:07.907Z | 74.417° E |
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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