STARLINK-36711, 68040
Orbit data source: Space-Track
STARLINK-36711, 68040 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 02 Mar 2026 UTC via an FALCON 9 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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68040 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
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 STARLINK-36711
1 68040U 26041A 26119.16668980 .00035312 00000-0 81748-3 0 9999
2 68040 53.1600 174.8320 0001301 88.7655 317.0999 15.42148481 5993Epoch: 2026-04-29T04:00Z
TLE epoch observation values (Epoch: 2026-04-29T04:00:01.998Z)
Latitude
35.16414°
Longitude
-70.64917°
Altitude
441.73 km
Speed
7.652 km/s
True Right ascension
13h 45m 57s
True Declination
34° 59' 42"
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
17:06:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
440.914 km
Perigee altitude
439.14 km
Semi-major axis
6,818.164 km
Eccentricity
0.00013
Inclination
53.16°
RAAN
174.832°
Arg. of periapsis
88.7655°
True anomaly
317.08975°
Mean anomaly
317.0999°
Eccentric anomaly
317.09483°
Mean motion
3.85516 °/min
Orbital period
93.38 mins
BSTAR
0.00081748
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Other satellites on launch #41 in the year 2026 (2026-03-02 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-36711 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 | 2026-04-29 12:02:17.646Z | 346.964° N | 2026-04-29 12:04:17.646Z | 30.84° NE | 18.726° | 2026-04-29 12:06:17.646Z | 69.968° E |
| 5 mins | 2026-04-29 13:39:17.646Z | 300.364° NW | 2026-04-29 13:41:17.646Z | 242.983° WSW | 41.702° | 2026-04-29 13:44:17.646Z | 142.62° SSE |
| 5 mins | 2026-04-30 06:26:17.646Z | 236.3° WSW | 2026-04-30 06:28:17.646Z | 262.147° W | 41.953° | 2026-04-30 06:31:17.646Z | 45.777° 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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