KUIPER-00593, 69278
Orbit data source: Space-Track
KUIPER-00593, 69278 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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69278 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-00593
1 69278U 26118M 26170.98211329 .00014491 00000-0 38981-3 0 9992
2 69278 51.8718 39.6641 0003710 165.9112 194.1979 15.38112556 4471Epoch: 2026-06-19T23:34Z
TLE epoch observation values (Epoch: 2026-06-19T23:34:14.588Z)
Latitude
-0.00002°
Longitude
137.90002°
Altitude
454.91 km
Speed
7.639 km/s
True Right ascension
02h 38m 39s
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
07:16:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.692 km
Perigee altitude
449.624 km
Semi-major axis
6,830.295 km
Eccentricity
0.00037
Inclination
51.8718°
RAAN
39.6641°
Arg. of periapsis
165.9112°
True anomaly
194.18748°
Mean anomaly
194.1979°
Eccentric anomaly
194.19269°
Mean motion
3.84489 °/min
Orbital period
93.63 mins
BSTAR
0.00038981
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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-00593 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 23:25:43.767Z | 348.126° N | 2026-06-20 23:26:43.767Z | 12.615° NNE | 22.835° | 2026-06-20 23:29:43.767Z | 79.593° E |
| 5 mins | 2026-06-21 01:02:43.767Z | 289.664° WNW | 2026-06-21 01:04:43.767Z | 227.527° WSW | 36.879° | 2026-06-21 01:07:43.767Z | 149.441° SSE |
| 5 mins | 2026-06-21 17:52:43.767Z | 237.445° WSW | 2026-06-21 17:54:43.767Z | 314.675° NW | 44.559° | 2026-06-21 17:57:43.767Z | 49.838° 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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