KUIPER-00543, 69612
Orbit data source: Space-Track
KUIPER-00543, 69612 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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69612 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: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00543
1 69612U 26140W 26178.50002315 .00020933 00000-0 58915-3 0 9995
2 69612 51.8799 348.9638 0006695 336.4326 195.9778 15.36411548 2072Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
5.94017°
Longitude
68.68514°
Altitude
461.318 km
Speed
7.635 km/s
True Right ascension
10h 57m 13s
True Declination
5° 54' 12"
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
09:21:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.773 km
Perigee altitude
452.62 km
Semi-major axis
6,835.334 km
Eccentricity
0.00067
Inclination
51.8799°
RAAN
348.9638°
Arg. of periapsis
336.4326°
True anomaly
195.9567°
Mean anomaly
195.9778°
Eccentric anomaly
195.96725°
Mean motion
3.84064 °/min
Orbital period
93.73 mins
BSTAR
0.00058915
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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-00543 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-28 13:57:43.828Z | 223.745° SW | 2026-06-28 14:00:43.828Z | 193.753° SSW | 40.839° | 2026-06-28 14:04:43.828Z | 56.069° ENE |
| 4 mins | 2026-06-28 15:37:43.828Z | 305.515° NW | 2026-06-28 15:38:43.828Z | 327.793° NNW | 19.885° | 2026-06-28 15:41:43.828Z | 28.013° NE |
| 5 mins | 2026-06-28 20:32:43.828Z | 311.18° NW | 2026-06-28 20:34:43.828Z | 90.417° ESE | 44.44° | 2026-06-28 20:37:43.828Z | 125.836° 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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