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 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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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 shape, 3.4 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00412
1 68927U 26098J 26171.37279957 .00022017 00000-0 60781-3 0 9990
2 68927 51.8789 51.8787 0002028 208.0768 152.0109 15.36997238 7841Epoch: 2026-06-20T08:56Z
TLE epoch observation values (Epoch: 2026-06-20T08:56:49.882Z)
Latitude
-0.00008°
Longitude
9.08243°
Altitude
456.982 km
Speed
7.639 km/s
True Right ascension
03h 27m 30s
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
07:21:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.846 km
Perigee altitude
454.075 km
Semi-major axis
6,833.598 km
Eccentricity
0.0002
Inclination
51.8789°
RAAN
51.8787°
Arg. of periapsis
208.0768°
True anomaly
152.0218°
Mean anomaly
152.0109°
Eccentric anomaly
152.01635°
Mean motion
3.8421 °/min
Orbital period
93.7 mins
BSTAR
0.00060781
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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 | 2026-06-21 01:02:03.995Z | 322.16° NNW | 2026-06-21 01:04:03.995Z | 6.117° NNE | 35.646° | 2026-06-21 01:07:03.995Z | 104.955° ESE |
| 4 mins | 2026-06-21 17:54:03.995Z | 170.976° S | 2026-06-21 17:55:03.995Z | 143.019° SSE | 25.834° | 2026-06-21 17:58:03.995Z | 75.431° E |
| 5 mins | 2026-06-21 19:31:03.995Z | 277.569° WNW | 2026-06-21 19:33:03.995Z | 339.607° N | 29.891° | 2026-06-21 19:36:03.995Z | 38.158° NE |
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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