STARLINK-37263, 68544
Orbit data source: Space-Track
STARLINK-37263, 68544 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Apr 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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68544 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 STARLINK-37263
1 68544U 26070C 26145.33862584 .00018007 00000-0 54281-3 0 9998
2 68544 53.1603 6.3053 0000905 115.1851 244.9245 15.34398458 8299Epoch: 2026-05-25T08:07Z
TLE epoch observation values (Epoch: 2026-05-25T08:07:37.272Z)
Latitude
-0.00007°
Longitude
1.4721°
Altitude
463.872 km
Speed
7.636 km/s
True Right ascension
00h 25m 13s
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
12:07:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.584 km
Perigee altitude
462.346 km
Semi-major axis
6,841.102 km
Eccentricity
0.00009
Inclination
53.1603°
RAAN
6.3053°
Arg. of periapsis
115.1851°
True anomaly
244.91511°
Mean anomaly
244.9245°
Eccentric anomaly
244.9198°
Mean motion
3.83578 °/min
Orbital period
93.85 mins
BSTAR
0.00054281
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Other satellites on launch #70 in the year 2026 (2026-04-02 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-37263 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 | 2026-05-26 17:07:49.798Z | 223.809° SW | 2026-05-26 17:10:49.798Z | 150.606° SSE | 44.348° | 2026-05-26 17:13:49.798Z | 53.08° ENE |
| 5 mins | 2026-05-26 23:42:49.798Z | 322.499° NNW | 2026-05-26 23:44:49.798Z | 41.566° NE | 41.614° | 2026-05-26 23:47:49.798Z | 118.255° SE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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