KUIPER-00192, 68575
Orbit data source: Space-Track
KUIPER-00192, 68575 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Sat, 04 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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68575 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
RCS unknown
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 KUIPER-00192
1 68575U 26072C 26138.83335647 -.00018606 00000-0 -18869-2 0 9994
2 68575 51.8981 323.1619 0005173 318.7695 184.0028 14.90058287 3218Epoch: 2026-05-18T20:00Z
TLE epoch observation values (Epoch: 2026-05-18T20:00:01.999Z)
Latitude
28.5192°
Longitude
-58.43597°
Altitude
602.684 km
Speed
7.56 km/s
True Right ascension
07h 52m 21s
True Declination
28° 22' 19"
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
09:57:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
601.816 km
Perigee altitude
594.598 km
Semi-major axis
6,976.344 km
Eccentricity
0.00052
Inclination
51.8981°
RAAN
323.1619°
Arg. of periapsis
318.7695°
True anomaly
183.99866°
Mean anomaly
184.0028°
Eccentric anomaly
184.00073°
Mean motion
3.72479 °/min
Orbital period
96.65 mins
BSTAR
-0.0018869
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Other satellites on launch #72 in the year 2026 (2026-04-04 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-00192 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-19 14:50:28.633Z | 219.653° SW | 2026-05-19 14:54:28.633Z | 149.855° SSE | 42.216° | 2026-05-19 14:58:28.633Z | 58.094° ENE |
| 6 mins | 2026-05-19 16:33:28.633Z | 291.929° WNW | 2026-05-19 16:35:28.633Z | 332.576° NNW | 25.857° | 2026-05-19 16:39:28.633Z | 38.003° NE |
| 5 mins | 2026-05-19 19:57:28.633Z | 340.671° N | 2026-05-19 19:59:28.633Z | 18.958° NNE | 22.83° | 2026-05-19 20:02:28.633Z | 69.749° E |
| 7 mins | 2026-05-19 21:37:28.633Z | 307.551° NW | 2026-05-19 21:40:28.633Z | 303.753° NW | 44.53° | 2026-05-19 21:44:28.633Z | 129.351° 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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