KUIPER-00269, 68587
Orbit data source: Space-Track
KUIPER-00269, 68587 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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68587 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00269
1 68587U 26072Q 26149.53416647 .00036859 00000-0 95526-3 0 9990
2 68587 51.8739 266.9174 0005152 300.3353 59.7124 15.38661686 8516Epoch: 2026-05-29T12:49Z
TLE epoch observation values (Epoch: 2026-05-29T12:49:11.983Z)
Latitude
-0.00003°
Longitude
-172.44572°
Altitude
449.056 km
Speed
7.645 km/s
True Right ascension
17h 47m 40s
True Declination
0° 00' 00"
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
00:53:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.051 km
Perigee altitude
447.015 km
Semi-major axis
6,828.67 km
Eccentricity
0.00052
Inclination
51.8739°
RAAN
266.9174°
Arg. of periapsis
300.3353°
True anomaly
59.7634°
Mean anomaly
59.7124°
Eccentric anomaly
59.7379°
Mean motion
3.84626 °/min
Orbital period
93.6 mins
BSTAR
0.00095526
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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-00269 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-30 15:45:44.669Z | 333.449° NNW | 2026-05-30 15:47:44.669Z | 11.385° NNE | 20.897° | 2026-05-30 15:50:44.669Z | 74.786° E |
| 5 mins | 2026-05-30 17:23:44.669Z | 296.344° NW | 2026-05-30 17:25:44.669Z | 236.293° WSW | 40.999° | 2026-05-30 17:28:44.669Z | 142.498° SSE |
| 5 mins | 2026-05-31 10:13:44.669Z | 226.473° WSW | 2026-05-31 10:15:44.669Z | 70.121° E | 43.092° | 2026-05-31 10:18:44.669Z | 53.747° ENE |
| 4 mins | 2026-05-31 11:51:44.669Z | 307.012° NW | 2026-05-31 11:52:44.669Z | 328.029° NNW | 18.414° | 2026-05-31 11:55:44.669Z | 27.056° NE |
| 4 mins | 2026-05-31 15:08:44.669Z | 347.268° N | 2026-05-31 15:10:44.669Z | 31.506° NE | 18.228° | 2026-05-31 15:12:44.669Z | 67.129° ENE |
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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