STARLINK-36869, 67954
Orbit data source: Space-Track
STARLINK-36869, 67954 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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67954 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-36869
1 67954U 26037Y 26171.43870889 .00012025 00000-0 44556-3 0 9990
2 67954 43.0044 330.5685 0001396 255.9572 104.1124 15.27596422 19053Epoch: 2026-06-20T10:31Z
TLE epoch observation values (Epoch: 2026-06-20T10:31:44.448Z)
Latitude
-0.00004°
Longitude
-96.02007°
Altitude
483.009 km
Speed
7.626 km/s
True Right ascension
22h 02m 16s
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
07:17:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.902 km
Perigee altitude
483.986 km
Semi-major axis
6,863.081 km
Eccentricity
0.00014
Inclination
43.0044°
RAAN
330.5685°
Arg. of periapsis
255.9572°
True anomaly
104.12791°
Mean anomaly
104.1124°
Eccentric anomaly
104.12016°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
0.00044556
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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-36869 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 20:27:35.864Z | 262.044° W | 2026-06-20 20:30:35.864Z | 205.86° SW | 18.981° | 2026-06-20 20:32:35.864Z | 170.69° S |
| 5 mins | 2026-06-21 13:24:35.864Z | 197.617° SSW | 2026-06-21 13:26:35.864Z | 153.604° SSE | 25.272° | 2026-06-21 13:29:35.864Z | 91.136° ESE |
| 5 mins | 2026-06-21 15:03:35.864Z | 260.228° W | 2026-06-21 15:05:35.864Z | 3.049° NNE | 44.349° | 2026-06-21 15:08:35.864Z | 70.29° E |
| 5 mins | 2026-06-21 16:42:35.864Z | 293.637° NW | 2026-06-21 16:44:35.864Z | 355.43° N | 38.013° | 2026-06-21 16:47:35.864Z | 75.971° E |
| 5 mins | 2026-06-21 18:21:35.864Z | 287.052° WNW | 2026-06-21 18:23:35.864Z | 269.075° W | 44.393° | 2026-06-21 18:26:35.864Z | 111.544° ESE |
| 4 mins | 2026-06-21 20:00:35.864Z | 252.428° W | 2026-06-21 20:02:35.864Z | 210.947° SW | 19.684° | 2026-06-21 20:04:35.864Z | 172.805° 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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