STARLINK-36426, 67560
Orbit data source: Space-Track
STARLINK-36426, 67560 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Thu, 22 Jan 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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67560 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 STARLINK-36426
1 67560U 26014AA 26171.22703297 .00012003 00000-0 37346-3 0 9998
2 67560 97.2861 57.9968 0001247 80.9862 279.1522 15.33450751 24491Epoch: 2026-06-20T05:26Z
TLE epoch observation values (Epoch: 2026-06-20T05:26:55.648Z)
Latitude
-0.00002°
Longitude
67.82025°
Altitude
468.502 km
Speed
7.632 km/s
True Right ascension
03h 51m 59s
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
07:24:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.322 km
Perigee altitude
461.616 km
Semi-major axis
6,840.606 km
Eccentricity
0.00012
Inclination
97.2861°
RAAN
57.9968°
Arg. of periapsis
80.9862°
True anomaly
279.13809°
Mean anomaly
279.1522°
Eccentric anomaly
279.14515°
Mean motion
3.8362 °/min
Orbital period
93.84 mins
BSTAR
0.00037346
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Other satellites on launch #14 in the year 2026 (2026-01-22 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.STARLINK-36426 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 05:29:52.979Z | 4.175° NNE | 2026-06-21 05:32:52.979Z | 265.958° W | 41.929° | 2026-06-21 05:35:52.979Z | 202.582° SW |
| 4 mins | 2026-06-21 16:03:52.979Z | 112.02° ESE | 2026-06-21 16:04:52.979Z | 78.886° E | 28.887° | 2026-06-21 16:07:52.979Z | 9.462° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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