STARLINK-36914, 67942
Orbit data source: Space-Track
STARLINK-36914, 67942 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 24 Feb 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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67942 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-36914
1 67942U 26037L 26171.43356693 .00019063 00000-0 70002-3 0 9993
2 67942 42.9987 330.5059 0000772 258.6572 101.4193 15.27600776 19050Epoch: 2026-06-20T10:24Z
TLE epoch observation values (Epoch: 2026-06-20T10:24:20.182Z)
Latitude
-0.00002°
Longitude
-94.22647°
Altitude
482.867 km
Speed
7.626 km/s
True Right ascension
22h 02m 01s
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
07:15:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.462 km
Perigee altitude
484.402 km
Semi-major axis
6,863.069 km
Eccentricity
0.00008
Inclination
42.9987°
RAAN
330.5059°
Arg. of periapsis
258.6572°
True anomaly
101.42797°
Mean anomaly
101.4193°
Eccentric anomaly
101.42364°
Mean motion
3.81738 °/min
Orbital period
94.31 mins
BSTAR
0.00070002
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Other satellites on launch #37 in the year 2026 (2026-02-24 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-36914 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 20:20:18.977Z | 258.215° W | 2026-06-20 20:22:18.977Z | 218.159° SW | 21.233° | 2026-06-20 20:25:18.977Z | 162.272° S |
| 4 mins | 2026-06-21 13:17:18.977Z | 186.887° SSW | 2026-06-21 13:19:18.977Z | 139.278° SSE | 22.945° | 2026-06-21 13:21:18.977Z | 98.845° ESE |
| 6 mins | 2026-06-21 14:55:18.977Z | 254.9° W | 2026-06-21 14:57:18.977Z | 267.794° W | 42.922° | 2026-06-21 15:01:18.977Z | 71.421° E |
| 6 mins | 2026-06-21 16:34:18.977Z | 288.439° WNW | 2026-06-21 16:37:18.977Z | 26.758° NE | 36.684° | 2026-06-21 16:40:18.977Z | 77.059° E |
| 6 mins | 2026-06-21 18:13:18.977Z | 288.601° WNW | 2026-06-21 18:16:18.977Z | 100.113° ESE | 44.042° | 2026-06-21 18:19:18.977Z | 108.024° ESE |
| 4 mins | 2026-06-21 19:53:18.977Z | 246.091° WSW | 2026-06-21 19:54:18.977Z | 223.602° SW | 21.462° | 2026-06-21 19:57:18.977Z | 163.634° S |
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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