KUIPER-00455, 68949
Orbit data source: Space-Track
KUIPER-00455, 68949 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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68949 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 KUIPER-00455
1 68949U 26098AG 26154.19741867 .00019336 00000-0 68397-3 0 9990
2 68949 51.8755 136.2140 0020086 95.7493 264.5781 15.28993499 5185Epoch: 2026-06-03T04:44Z
TLE epoch observation values (Epoch: 2026-06-03T04:44:16.973Z)
Latitude
0°
Longitude
173.48379°
Altitude
480.909 km
Speed
7.626 km/s
True Right ascension
09h 04m 51s
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
03:00:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.059 km
Perigee altitude
465.511 km
Semi-major axis
6,857.422 km
Eccentricity
0.00201
Inclination
51.8755°
RAAN
136.214°
Arg. of periapsis
95.7493°
True anomaly
264.34902°
Mean anomaly
264.5781°
Eccentric anomaly
264.46355°
Mean motion
3.8221 °/min
Orbital period
94.19 mins
BSTAR
0.00068397
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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-00455 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 | 2026-06-06 23:53:10.900Z | 198.498° SSW | 2026-06-06 23:56:10.900Z | 116.397° SE | 30.67° | 2026-06-06 23:58:10.900Z | 73.431° E |
| 4 mins | 2026-06-07 01:32:10.900Z | 286.566° WNW | 2026-06-07 01:34:10.900Z | 343.534° N | 26.687° | 2026-06-07 01:36:10.900Z | 27.678° NE |
| 5 mins | 2026-06-07 06:29:10.900Z | 330.349° NNW | 2026-06-07 06:31:10.900Z | 52.948° ENE | 36.463° | 2026-06-07 06:34:10.900Z | 108.943° ESE |
| 4 mins | 2026-06-07 08:07:10.900Z | 261.475° W | 2026-06-07 08:09:10.900Z | 217.527° SW | 18.496° | 2026-06-07 08:11:10.900Z | 182.785° SSW |
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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