KUIPER-00595, 69280
Orbit data source: Space-Track
KUIPER-00595, 69280 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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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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00595
1 69280U 26118P 26171.36509178 .00022302 00000-0 58491-3 0 9998
2 69280 51.8720 37.7323 0001318 157.6610 202.4435 15.38576839 4508Epoch: 2026-06-20T08:45Z
TLE epoch observation values (Epoch: 2026-06-20T08:45:43.929Z)
Latitude
-0.00002°
Longitude
-2.28152°
Altitude
451.912 km
Speed
7.642 km/s
True Right ascension
02h 30m 55s
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
07:11:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.684 km
Perigee altitude
449.884 km
Semi-major axis
6,828.921 km
Eccentricity
0.00013
Inclination
51.872°
RAAN
37.7323°
Arg. of periapsis
157.661°
True anomaly
202.43773°
Mean anomaly
202.4435°
Eccentric anomaly
202.44062°
Mean motion
3.84605 °/min
Orbital period
93.6 mins
BSTAR
0.00058491
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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-00595 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 23:14:57.660Z | 346.358° N | 2026-06-20 23:16:57.660Z | 34.865° NE | 20.608° | 2026-06-20 23:18:57.660Z | 72.94° E |
| 5 mins | 2026-06-21 00:51:57.660Z | 297.744° NW | 2026-06-21 00:53:57.660Z | 249.597° W | 40.664° | 2026-06-21 00:56:57.660Z | 142.231° SSE |
| 5 mins | 2026-06-21 17:41:57.660Z | 226.088° WSW | 2026-06-21 17:43:57.660Z | 106.079° ESE | 44.536° | 2026-06-21 17:46:57.660Z | 54.227° 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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