STARLINK-33992, 64026
Orbit data source: Space-Track
STARLINK-33992, 64026 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 16 May 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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64026 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-33992
1 64026U 25102E 26171.40958147 .00002803 00000-0 24258-3 0 9990
2 64026 69.9997 215.6601 0003702 268.0284 92.0451 14.98336409 61423Epoch: 2026-06-20T09:49Z
TLE epoch observation values (Epoch: 2026-06-20T09:49:47.839Z)
Latitude
-0.00007°
Longitude
159.58614°
Altitude
574.553 km
Speed
7.574 km/s
True Right ascension
14h 22m 38s
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
08:32:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.557 km
Perigee altitude
567.412 km
Semi-major axis
6,948.121 km
Eccentricity
0.00037
Inclination
69.9997°
RAAN
215.6601°
Arg. of periapsis
268.0284°
True anomaly
92.08749°
Mean anomaly
92.0451°
Eccentric anomaly
92.0663°
Mean motion
3.7475 °/min
Orbital period
96.06 mins
BSTAR
0.00024258
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Other satellites on launch #102 in the year 2025 (2025-05-16 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-33992 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 | 2026-06-21 03:34:46.290Z | 157.164° SSE | 2026-06-21 03:37:46.290Z | 107.644° ESE | 22.12° | 2026-06-21 03:40:46.290Z | 55.818° ENE |
| 5 mins | 2026-06-21 05:13:46.290Z | 255.359° W | 2026-06-21 05:15:46.290Z | 295.21° NW | 24.896° | 2026-06-21 05:18:46.290Z | 354.309° N |
| 6 mins | 2026-06-21 13:37:46.290Z | 354.725° N | 2026-06-21 13:39:46.290Z | 41.492° NE | 37.376° | 2026-06-21 13:43:46.290Z | 138.14° SSE |
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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