KUIPER-00234, 68581
Orbit data source: Space-Track
KUIPER-00234, 68581 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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68581 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: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00234
1 68581U 26072J 26150.16668980 .00013262 00000-0 17373-2 0 9990
2 68581 51.8992 269.2823 0000732 52.4701 313.4861 14.80607261 5834Epoch: 2026-05-30T04:00Z
TLE epoch observation values (Epoch: 2026-05-30T04:00:01.998Z)
Latitude
4.63142°
Longitude
-34.79045°
Altitude
627.32 km
Speed
7.547 km/s
True Right ascension
18h 11m 37s
True Declination
4° 36' 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
00:42:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.372 km
Perigee altitude
627.347 km
Semi-major axis
7,005.996 km
Eccentricity
0.00007
Inclination
51.8992°
RAAN
269.2823°
Arg. of periapsis
52.4701°
True anomaly
313.48001°
Mean anomaly
313.4861°
Eccentric anomaly
313.48306°
Mean motion
3.70116 °/min
Orbital period
97.27 mins
BSTAR
0.0017373
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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-00234 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 | 2026-05-30 15:44:32.314Z | 325.893° NNW | 2026-05-30 15:47:32.314Z | 10.985° NNE | 22.988° | 2026-05-30 15:51:32.314Z | 74.413° E |
| 7 mins | 2026-05-30 17:26:32.314Z | 308.323° NW | 2026-05-30 17:29:32.314Z | 316.81° NNW | 44.448° | 2026-05-30 17:33:32.314Z | 128.067° SE |
| 5 mins | 2026-05-31 09:17:32.314Z | 162.84° S | 2026-05-31 09:19:32.314Z | 130.212° SE | 19.219° | 2026-05-31 09:22:32.314Z | 85.064° E |
| 7 mins | 2026-05-31 10:57:32.314Z | 244.408° WSW | 2026-05-31 11:00:32.314Z | 312.572° NW | 42.826° | 2026-05-31 11:04:32.314Z | 47.261° ENE |
| 5 mins | 2026-05-31 12:40:32.314Z | 306.5° NW | 2026-05-31 12:42:32.314Z | 340.481° N | 20.964° | 2026-05-31 12:45:32.314Z | 29.431° NE |
| 5 mins | 2026-05-31 14:23:32.314Z | 335.926° NNW | 2026-05-31 14:25:32.314Z | 7.886° NNE | 17.674° | 2026-05-31 14:28:32.314Z | 50.186° ENE |
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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