KUIPER-00522, 69602
Orbit data source: Space-Track
KUIPER-00522, 69602 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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69602 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-00522
1 69602U 26140L 26178.50002315 .00025708 00000-0 67882-3 0 9992
2 69602 51.8792 348.7323 0013997 197.7830 90.2353 15.38193488 2252Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-48.54235°
Longitude
-168.93647°
Altitude
468.03 km
Speed
7.632 km/s
True Right ascension
19h 06m 44s
True Declination
-48° 21' 52"
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
10:23:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.478 km
Perigee altitude
442.357 km
Semi-major axis
6,830.054 km
Eccentricity
0.0014
Inclination
51.8792°
RAAN
348.7323°
Arg. of periapsis
197.783°
True anomaly
90.39569°
Mean anomaly
90.2353°
Eccentric anomaly
90.3155°
Mean motion
3.84509 °/min
Orbital period
93.63 mins
BSTAR
0.00067882
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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-00522 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 13:25:29.389Z | 196.452° SSW | 2026-06-28 13:28:29.389Z | 123.367° SE | 28.72° | 2026-06-28 13:30:29.389Z | 77.205° E |
| 5 mins | 2026-06-28 15:03:29.389Z | 275.665° WNW | 2026-06-28 15:05:29.389Z | 323.969° NNW | 28.051° | 2026-06-28 15:08:29.389Z | 33.664° NE |
| 4 mins | 2026-06-28 19:59:29.389Z | 337.874° N | 2026-06-28 20:00:29.389Z | 8.935° NNE | 32.877° | 2026-06-28 20:03:29.389Z | 99.736° ESE |
| 4 mins | 2026-06-28 21:36:29.389Z | 267.927° W | 2026-06-28 21:38:29.389Z | 221.382° SW | 20.824° | 2026-06-28 21:40:29.389Z | 181.002° 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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