POLARIS DAWN DEB, 61073 (Decayed)
Orbit data source: Space-Track
POLARIS DAWN DEB, 61073 was space debris in LEO originally from a launch on Tue, 10 Sep 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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61073 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
10 months ago
Origin
Manufacturer
SpaceX
Mission
Decayed spacecraft
Bus & Motor
DRAGON SM, Unknown motor
Mass
Wet unknown, ~2,300 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.9 m
Radar Cross Section
16.128 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 10 months ago
0 POLARIS DAWN DEB
1 61073U 24161B 24273.53565471 .12108337 11959-4 86807-3 0 9991
2 61073 51.6411 286.9673 0038217 121.3262 11.7754 16.35852185 2298Epoch: 2024-09-29T12:51Z
TLE epoch observation values (Epoch: 2024-09-29T12:51:20.566Z)
Latitude
34.98988°
Longitude
-128.06386°
Altitude
154.739 km
Speed
7.833 km/s
True Right ascension
04h 54m 11s
True Declination
34° 48' 49"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
Orbital elements
Apogee altitude
202.439 km
Perigee altitude
152.332 km
Semi-major axis
6,555.523 km
Eccentricity
0.00382
Inclination
51.6411°
RAAN
286.9673°
Arg. of periapsis
121.3262°
True anomaly
11.86519°
Mean anomaly
11.7754°
Eccentric anomaly
11.82025°
Mean motion
4.08914 °/min
Orbital period
88.04 mins
BSTAR
0.00086807
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Other satellites on launch #161 in the year 2024 (2024-09-10 UTC)
POLARIS DAWN DEB Visibility
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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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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Authenticating...
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