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: 21 hours ago
TLE from 21 hours ago
0 LIZZIESAT
1 59132U 24043AL 25318.61368561 .00006192 00000-0 24872-3 0 9992
2 59132 97.5357 87.1956 0009800 281.6006 78.4132 15.25279552 94207Epoch: 2025-11-14T14:43Z
TLE epoch observation values (Epoch: 2025-11-14T14:43:42.436Z)
Latitude
0.00003°
Longitude
172.31412°
Altitude
491.694 km
Speed
7.62 km/s
True Right ascension
05h 48m 46s
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
08:25:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.638 km
Perigee altitude
480.183 km
Semi-major axis
6,865.048 km
Eccentricity
0.00098
Inclination
97.5357°
RAAN
87.1956°
Arg. of periapsis
281.6006°
True anomaly
78.52324°
Mean anomaly
78.4132°
Eccentric anomaly
78.46822°
Mean motion
3.81573 °/min
Orbital period
94.35 mins
BSTAR
0.00024872
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-15 21:12:45.511Z | 31.181° NE | 2025-11-15 21:15:45.511Z | 111.382° ESE | 33.259° | 2025-11-15 21:18:45.511Z | 170.126° S |
| 4 mins | 2025-11-16 09:22:45.511Z | 217.005° SW | 2025-11-16 09:24:45.511Z | 267.947° W | 25.216° | 2025-11-16 09:26:45.511Z | 313.608° NW |
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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