KUIPER-00423, 69592
Orbit data source: Space-Track
KUIPER-00423, 69592 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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69592 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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00423
1 69592U 26140A 26177.25002315 .00023935 00000-0 63333-3 0 9998
2 69592 51.8819 354.7874 0014064 196.4836 3.4579 15.38169670 1303Epoch: 2026-06-26T06:00Z
TLE epoch observation values (Epoch: 2026-06-26T06:00:02.000Z)
Latitude
-15.73473°
Longitude
-176.90313°
Altitude
446.042 km
Speed
7.65 km/s
True Right ascension
12h 29m 56s
True Declination
-15° 38' 28"
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
05:39:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.593 km
Perigee altitude
442.382 km
Semi-major axis
6,830.125 km
Eccentricity
0.00141
Inclination
51.8819°
RAAN
354.7874°
Arg. of periapsis
196.4836°
True anomaly
3.46764°
Mean anomaly
3.4579°
Eccentric anomaly
3.46277°
Mean motion
3.84503 °/min
Orbital period
93.63 mins
BSTAR
0.00063333
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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-00423 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-26 19:35:48.886Z | 337.212° NNW | 2026-06-26 19:37:48.886Z | 14.066° NNE | 16.993° | 2026-06-26 19:39:48.886Z | 54.213° ENE |
| 5 mins | 2026-06-26 21:13:48.886Z | 312.734° NW | 2026-06-26 21:15:48.886Z | 2.374° NNE | 43.925° | 2026-06-26 21:18:48.886Z | 122.787° SE |
| 5 mins | 2026-06-27 14:03:48.886Z | 202.478° SSW | 2026-06-27 14:05:48.886Z | 140.224° SSE | 36.33° | 2026-06-27 14:08:48.886Z | 64.879° ENE |
| 4 mins | 2026-06-27 15:41:48.886Z | 291.839° WNW | 2026-06-27 15:43:48.886Z | 343.855° N | 23.772° | 2026-06-27 15:45:48.886Z | 25.985° NE |
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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