KUIPER-00524, 68892
Orbit data source: Space-Track
KUIPER-00524, 68892 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 28 Apr 2026 UTC via an ATLAS V 551 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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68892 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 shape, 3.4 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00524
1 68892U 26095AE 26171.41668980 -.00024669 00000-0 -12635-2 0 9992
2 68892 51.8959 227.6660 0002022 39.2842 282.2370 15.15805737 4982Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-29.53232°
Longitude
142.80526°
Altitude
527.064 km
Speed
7.6 km/s
True Right ascension
13h 25m 46s
True Declination
-29° 22' 48"
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
07:19:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.387 km
Perigee altitude
517.598 km
Semi-major axis
6,897.129 km
Eccentricity
0.0002
Inclination
51.8959°
RAAN
227.666°
Arg. of periapsis
39.2842°
True anomaly
282.21435°
Mean anomaly
282.237°
Eccentric anomaly
282.22568°
Mean motion
3.78914 °/min
Orbital period
95.01 mins
BSTAR
-0.0012635
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Other satellites on launch #95 in the year 2026 (2026-04-28 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-00524 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 | 2026-06-21 05:18:55.523Z | 164.465° S | 2026-06-21 05:20:55.523Z | 129.684° SE | 16.881° | 2026-06-21 05:22:55.523Z | 94.598° ESE |
| 6 mins | 2026-06-21 06:56:55.523Z | 246.773° WSW | 2026-06-21 06:59:55.523Z | 355.644° N | 40.86° | 2026-06-21 07:02:55.523Z | 45.819° ENE |
| 4 mins | 2026-06-21 08:37:55.523Z | 319.753° NNW | 2026-06-21 08:38:55.523Z | 339.009° N | 17.679° | 2026-06-21 08:41:55.523Z | 29.536° NE |
| 5 mins | 2026-06-21 11:56:55.523Z | 332.967° NNW | 2026-06-21 11:58:55.523Z | 13.225° NNE | 26.058° | 2026-06-21 12:01:55.523Z | 80.797° E |
| 6 mins | 2026-06-21 13:35:55.523Z | 290.886° WNW | 2026-06-21 13:38:55.523Z | 199.417° SSW | 35.247° | 2026-06-21 13:41:55.523Z | 150.365° SSE |
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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