STARLINK-36648, 67825
Orbit data source: Space-Track
STARLINK-36648, 67825 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 16 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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67825 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-36648
1 67825U 26033E 26171.38166187 .00013698 00000-0 50620-3 0 9992
2 67825 43.0055 46.7263 0001179 287.1293 72.9429 15.27590814 20383Epoch: 2026-06-20T09:09Z
TLE epoch observation values (Epoch: 2026-06-20T09:09:35.585Z)
Latitude
-0.00006°
Longitude
0.73087°
Altitude
482.556 km
Speed
7.626 km/s
True Right ascension
03h 06m 54s
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
08:43:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.77 km
Perigee altitude
484.152 km
Semi-major axis
6,863.098 km
Eccentricity
0.00012
Inclination
43.0055°
RAAN
46.7263°
Arg. of periapsis
287.1293°
True anomaly
72.95582°
Mean anomaly
72.9429°
Eccentric anomaly
72.94936°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.0005062
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Other satellites on launch #33 in the year 2026 (2026-02-16 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-36648 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 22:03:09.087Z | 284.057° WNW | 2026-06-20 22:07:09.087Z | 25.933° NE | 36.928° | 2026-06-20 22:10:09.087Z | 77.975° E |
| 6 mins | 2026-06-20 23:43:09.087Z | 287.695° WNW | 2026-06-20 23:46:09.087Z | 119.571° SE | 44.17° | 2026-06-20 23:49:09.087Z | 110.519° ESE |
| 4 mins | 2026-06-21 01:23:09.087Z | 244.955° WSW | 2026-06-21 01:24:09.087Z | 223.543° SW | 19.992° | 2026-06-21 01:27:09.087Z | 166.304° S |
| 5 mins | 2026-06-21 18:19:09.087Z | 192.352° SSW | 2026-06-21 18:21:09.087Z | 145.773° SSE | 24.279° | 2026-06-21 18:24:09.087Z | 89.787° E |
| 6 mins | 2026-06-21 19:57:09.087Z | 256.547° W | 2026-06-21 20:00:09.087Z | 46.19° ENE | 43.378° | 2026-06-21 20:03:09.087Z | 70.907° E |
| 5 mins | 2026-06-21 21:37:09.087Z | 296.095° NW | 2026-06-21 21:39:09.087Z | 12.582° NNE | 37.785° | 2026-06-21 21:42:09.087Z | 76.641° E |
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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