KUIPER-00592, 69277
Orbit data source: Space-Track
KUIPER-00592, 69277 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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69277 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: 19 hours ago
TLE from 19 hours ago
0 KUIPER-00592
1 69277U 26118L 26171.04629024 .00019766 00000-0 52666-3 0 9990
2 69277 51.8715 39.3448 0003485 144.9717 215.1500 15.38165452 4428Epoch: 2026-06-20T01:06Z
TLE epoch observation values (Epoch: 2026-06-20T01:06:39.476Z)
Latitude
-0.00002°
Longitude
114.41377°
Altitude
454.244 km
Speed
7.64 km/s
True Right ascension
02h 37m 22s
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
07:13:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.382 km
Perigee altitude
449.621 km
Semi-major axis
6,830.139 km
Eccentricity
0.00035
Inclination
51.8715°
RAAN
39.3448°
Arg. of periapsis
144.9717°
True anomaly
215.12702°
Mean anomaly
215.15°
Eccentric anomaly
215.13851°
Mean motion
3.84502 °/min
Orbital period
93.63 mins
BSTAR
0.00052666
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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-00592 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 23:23:59.713Z | 339.987° N | 2026-06-20 23:25:59.713Z | 28.018° NE | 23.002° | 2026-06-20 23:27:59.713Z | 73.076° E |
| 4 mins | 2026-06-21 01:01:59.713Z | 284.251° WNW | 2026-06-21 01:03:59.713Z | 194.4° SSW | 35.91° | 2026-06-21 01:05:59.713Z | 151.396° SSE |
| 5 mins | 2026-06-21 17:50:59.713Z | 235.366° WSW | 2026-06-21 17:52:59.713Z | 249.295° W | 42.065° | 2026-06-21 17:55:59.713Z | 49.807° 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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