FALCON 9 R/B, 61911
Orbit data source: Space-Track
FALCON 9 R/B, 61911 is space debris in HEO originally from a launch on Mon, 11 Nov 2024 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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61911 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FALCON 9 R/B
1 61911U 24206B 25248.66287222 .00008217 00000-0 11548-2 0 9997
2 61911 27.4928 34.3332 7233921 7.6839 358.9998 2.35637945 6944
Epoch: 2025-09-05T15:54Z
TLE epoch observation values (Epoch: 2025-09-05T15:54:32.159Z)
Latitude
0.00056°
Longitude
170.68265°
Altitude
258.294 km
Speed
10.169 km/s
True Right ascension
02h 17m 17s
True Declination
0° 00' 02"
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
20:07:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,739.253 km
Perigee altitude
221.287 km
Semi-major axis
23,858.407 km
Eccentricity
0.72339
Inclination
27.4928°
RAAN
34.3332°
Arg. of periapsis
7.6839°
True anomaly
351.0054°
Mean anomaly
358.9998°
Eccentric anomaly
356.39029°
Mean motion
0.58895 °/min
Orbital period
611.25 mins
BSTAR
0.0011548
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Other satellites on launch #206 in the year 2024 (2024-11-11 UTC)
FALCON 9 R/B Visibility forecast
Observer location: undefined°, undefined°
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. |
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474 mins | 2025-09-07 19:11:55.755Z | 267.383° W | 2025-09-07 19:52:55.755Z | 200.901° SSW | 40.357° | 2025-09-08 03:05:55.755Z | 218.475° SW |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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