STARLINK-11396, 62015
Orbit data source: Space-Track
STARLINK-11396, 62015 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 18 Nov 2024 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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62015 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-11396
1 62015U 24213H 25259.26990046 .00132904 00000-0 10827-2 0 9994
2 62015 53.1567 180.8604 0000926 101.1425 258.9698 15.69747112 47529Epoch: 2025-09-16T06:28Z
TLE epoch observation values (Epoch: 2025-09-16T06:28:39.399Z)
Latitude
0.00004°
Longitude
88.23365°
Altitude
360.655 km
Speed
7.694 km/s
True Right ascension
12h 03m 26s
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
14:26:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.506 km
Perigee altitude
359.258 km
Semi-major axis
6,738.019 km
Eccentricity
0.00009
Inclination
53.1567°
RAAN
180.8604°
Arg. of periapsis
101.1425°
True anomaly
258.95939°
Mean anomaly
258.9698°
Eccentric anomaly
258.96459°
Mean motion
3.92414 °/min
Orbital period
91.74 mins
BSTAR
0.0010827
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Other satellites on launch #213 in the year 2024 (2024-11-18 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-11396 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 21:57:36.121Z | 247.401° WSW | 2025-09-16 21:59:36.121Z | 318.863° NNW | 39.353° | 2025-09-16 22:01:36.121Z | 37.231° NE |
| 4 mins | 2025-09-17 04:22:36.121Z | 311.371° NW | 2025-09-17 04:24:36.121Z | 122.465° SE | 43.071° | 2025-09-17 04:26:36.121Z | 129.598° SE |
| 4 mins | 2025-09-17 20:51:36.121Z | 193.197° SSW | 2025-09-17 20:52:36.121Z | 158.898° S | 32.462° | 2025-09-17 20:55:36.121Z | 63.677° ENE |
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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