STARLINK-11288, 61002
Orbit data source: Space-Track
STARLINK-11288, 61002 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 05 Sep 2024 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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61002 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MD, Unknown motor
Mass
960 kg wet, ~910 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 STARLINK-11288
1 61002U 24158N 25258.70667567 .00002018 00000-0 21495-4 0 9991
2 61002 53.1600 63.7169 0001088 81.3578 278.7563 15.69725393 60102Epoch: 2025-09-15T16:57Z
TLE epoch observation values (Epoch: 2025-09-15T16:57:36.777Z)
Latitude
-0.00006°
Longitude
174.40615°
Altitude
360.486 km
Speed
7.694 km/s
True Right ascension
04h 14m 52s
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
00:40:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.676 km
Perigee altitude
359.21 km
Semi-major axis
6,738.08 km
Eccentricity
0.00011
Inclination
53.16°
RAAN
63.7169°
Arg. of periapsis
81.3578°
True anomaly
278.74398°
Mean anomaly
278.7563°
Eccentric anomaly
278.75014°
Mean motion
3.92409 °/min
Orbital period
91.74 mins
BSTAR
0.000021495
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Other satellites on launch #158 in the year 2024 (2024-09-05 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-11288 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-16 12:59:06.578Z | 183.949° SSW | 2025-09-16 13:01:06.578Z | 137.921° SSE | 21.072° | 2025-09-16 13:03:06.578Z | 84.657° E |
| 4 mins | 2025-09-16 14:35:06.578Z | 280.76° WNW | 2025-09-16 14:36:06.578Z | 309.29° NW | 24.488° | 2025-09-16 14:39:06.578Z | 30.081° NE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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