KUIPER-00370, 68919
Orbit data source: Space-Track
KUIPER-00370, 68919 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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68919 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00370
1 68919U 26098A 26140.58335648 .00043001 00000-0 14211-2 0 9992
2 68919 51.8714 201.0654 0015708 57.1984 267.0802 15.30834749 4041Epoch: 2026-05-20T14:00Z
TLE epoch observation values (Epoch: 2026-05-20T14:00:01.999Z)
Latitude
-27.66793°
Longitude
88.65844°
Altitude
482 km
Speed
7.624 km/s
True Right ascension
11h 47m 37s
True Declination
-27° 31' 16"
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
08:08:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.549 km
Perigee altitude
463.023 km
Semi-major axis
6,851.923 km
Eccentricity
0.00157
Inclination
51.8714°
RAAN
201.0654°
Arg. of periapsis
57.1984°
True anomaly
266.90045°
Mean anomaly
267.0802°
Eccentric anomaly
266.99032°
Mean motion
3.8267 °/min
Orbital period
94.08 mins
BSTAR
0.0014211
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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-00370 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 | 2026-05-21 05:59:08.344Z | 182.789° SSW | 2026-05-21 06:01:08.344Z | 143.619° SSE | 22.371° | 2026-05-21 06:04:08.344Z | 79.827° E |
| 5 mins | 2026-05-21 07:37:08.344Z | 266.067° W | 2026-05-21 07:39:08.344Z | 318.572° NNW | 32.958° | 2026-05-21 07:42:08.344Z | 36.924° NE |
| 5 mins | 2026-05-21 12:34:08.344Z | 335.526° NNW | 2026-05-21 12:36:08.344Z | 33.868° NE | 30.103° | 2026-05-21 12:39:08.344Z | 95.976° ESE |
| 5 mins | 2026-05-21 14:12:08.344Z | 273.581° WNW | 2026-05-21 14:14:08.344Z | 219.408° SW | 26.82° | 2026-05-21 14:17:08.344Z | 163.488° S |
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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