STARLINK-36940, 68027
Orbit data source: Space-Track
STARLINK-36940, 68027 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sun, 01 Mar 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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68027 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-36940
1 68027U 26040N 26171.43420889 .00017556 00000-0 54493-3 0 9992
2 68027 97.2825 120.1563 0002770 77.9522 282.2031 15.33438320 17215Epoch: 2026-06-20T10:25Z
TLE epoch observation values (Epoch: 2026-06-20T10:25:15.648Z)
Latitude
-0°
Longitude
55.19221°
Altitude
468.275 km
Speed
7.632 km/s
True Right ascension
08h 00m 37s
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
07:13:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.401 km
Perigee altitude
460.611 km
Semi-major axis
6,840.643 km
Eccentricity
0.00028
Inclination
97.2825°
RAAN
120.1563°
Arg. of periapsis
77.9522°
True anomaly
282.17207°
Mean anomaly
282.2031°
Eccentric anomaly
282.18759°
Mean motion
3.83617 °/min
Orbital period
93.84 mins
BSTAR
0.00054493
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Other satellites on launch #40 in the year 2026 (2026-03-01 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-36940 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 21:30:52.440Z | 223.24° SW | 2026-06-20 21:32:52.440Z | 259.591° W | 16.612° | 2026-06-20 21:34:52.440Z | 300.506° NW |
| 4 mins | 2026-06-21 08:55:52.440Z | 52.34° ENE | 2026-06-21 08:57:52.440Z | 110.187° ESE | 25.386° | 2026-06-21 08:59:52.440Z | 152.882° SSE |
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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