LIZZIESAT, 59132
Orbit data source: Space-Track
LIZZIESAT, 59132 is a payload satellite owned by Sidus Space (US) in SSO that was launched on Mon, 04 Mar 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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59132 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Sidus Space
Mission
Operational Commercial Technology
Bus & Motor
LIZZIESAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Oct Cyl + 8 Pan, 0.7 m
Radar Cross Section
1.008 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LIZZIESAT
1 59132U 24043AL 25363.93720485 .00005792 00000-0 22885-3 0 9991
2 59132 97.5384 132.8699 0012333 117.4556 242.7937 15.25833056101113Epoch: 2025-12-29T22:29Z
TLE epoch observation values (Epoch: 2025-12-29T22:29:34.499Z)
Latitude
-0.00005°
Longitude
56.84849°
Altitude
495.26 km
Speed
7.615 km/s
True Right ascension
08h 51m 28s
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
08:14:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.713 km
Perigee altitude
476.784 km
Semi-major axis
6,863.386 km
Eccentricity
0.00123
Inclination
97.5384°
RAAN
132.8699°
Arg. of periapsis
117.4556°
True anomaly
242.6681°
Mean anomaly
242.7937°
Eccentric anomaly
242.73089°
Mean motion
3.81712 °/min
Orbital period
94.31 mins
BSTAR
0.00022885
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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LIZZIESAT 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-30 09:38:24.553Z | 219.774° SW | 2025-12-30 09:40:24.553Z | 255.909° W | 18.388° | 2025-12-30 09:43:24.553Z | 312.995° NW |
| 5 mins | 2025-12-30 21:06:24.553Z | 45.617° ENE | 2025-12-30 21:08:24.553Z | 93.611° ESE | 25.961° | 2025-12-30 21:11:24.553Z | 157.536° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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