KUIPER-00490, 69595
Orbit data source: Space-Track
KUIPER-00490, 69595 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Wed, 17 Jun 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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69595 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: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00490
1 69595U 26140D 26178.50002315 .00021493 00000-0 58470-3 0 9993
2 69595 51.8791 348.8823 0005818 267.4908 305.2061 15.37458297 2731Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-25.30401°
Longitude
94.91045°
Altitude
458.582 km
Speed
7.639 km/s
True Right ascension
12h 42m 07s
True Declination
-25° 09' 56"
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
10:51:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.069 km
Perigee altitude
450.119 km
Semi-major axis
6,832.231 km
Eccentricity
0.00058
Inclination
51.8791°
RAAN
348.8823°
Arg. of periapsis
267.4908°
True anomaly
305.1516°
Mean anomaly
305.2061°
Eccentric anomaly
305.17885°
Mean motion
3.84326 °/min
Orbital period
93.67 mins
BSTAR
0.0005847
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Other satellites on launch #140 in the year 2026 (2026-06-17 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-00490 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 | 2026-06-28 13:46:45.659Z | 211.196° SW | 2026-06-28 13:48:45.659Z | 170.716° S | 37.055° | 2026-06-28 13:51:45.659Z | 64.518° ENE |
| 4 mins | 2026-06-28 15:25:45.659Z | 303.947° NW | 2026-06-28 15:26:45.659Z | 329.436° NNW | 22.544° | 2026-06-28 15:29:45.659Z | 30.72° NE |
| 5 mins | 2026-06-28 20:20:45.659Z | 322.797° NNW | 2026-06-28 20:22:45.659Z | 79.556° E | 39.856° | 2026-06-28 20:25:45.659Z | 118.24° 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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