KUIPER-00590, 69276
Orbit data source: Space-Track
KUIPER-00590, 69276 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Fri, 29 May 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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69276 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 KUIPER-00590
1 69276U 26118K 26170.98416114 .00019553 00000-0 52417-3 0 9993
2 69276 51.8693 39.6781 0004035 170.0397 190.0671 15.37983586 4415Epoch: 2026-06-19T23:37Z
TLE epoch observation values (Epoch: 2026-06-19T23:37:11.522Z)
Latitude
0.00001°
Longitude
137.1748°
Altitude
455.549 km
Speed
7.639 km/s
True Right ascension
02h 38m 42s
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
07:13:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.297 km
Perigee altitude
449.784 km
Semi-major axis
6,830.677 km
Eccentricity
0.0004
Inclination
51.8693°
RAAN
39.6781°
Arg. of periapsis
170.0397°
True anomaly
190.05902°
Mean anomaly
190.0671°
Eccentric anomaly
190.06306°
Mean motion
3.84457 °/min
Orbital period
93.64 mins
BSTAR
0.00052417
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Other satellites on launch #118 in the year 2026 (2026-05-29 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-00590 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 | 2026-06-20 23:28:33.032Z | 340.752° N | 2026-06-20 23:30:33.032Z | 31.715° NE | 24.033° | 2026-06-20 23:32:33.032Z | 76.518° E |
| 4 mins | 2026-06-21 01:06:33.032Z | 278.857° WNW | 2026-06-21 01:07:33.032Z | 247.404° WSW | 33.999° | 2026-06-21 01:10:33.032Z | 154.228° SSE |
| 6 mins | 2026-06-21 17:55:33.032Z | 239.176° WSW | 2026-06-21 17:57:33.032Z | 263.031° W | 41.29° | 2026-06-21 18:01:33.032Z | 49.492° 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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