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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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: 7 hours ago
TLE from 7 hours ago
0 LIZZIESAT
1 59132U 24043AL 26255.93053598 .00003062 00000-0 11482-3 0 9995
2 59132 97.5764 33.0589 0009251 300.6584 59.3743 15.28014075140336Epoch: 2026-09-12T22:19Z
TLE epoch observation values (Epoch: 2026-09-12T22:19:58.308Z)
Latitude
0.00001°
Longitude
66.13348°
Altitude
481.617 km
Speed
7.626 km/s
True Right ascension
02h 12m 14s
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
22:14:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.055 km
Perigee altitude
472.369 km
Semi-major axis
6,856.849 km
Eccentricity
0.00093
Inclination
97.5764°
RAAN
33.0589°
Arg. of periapsis
300.6584°
True anomaly
59.46558°
Mean anomaly
59.3743°
Eccentric anomaly
59.41993°
Mean motion
3.82258 °/min
Orbital period
94.18 mins
BSTAR
0.00011482
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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 | 2026-09-13 09:27:07.759Z | 177.481° S | 2026-09-13 09:30:07.759Z | 226.531° WSW | 58.766° | 2026-09-13 09:33:07.759Z | 338.216° N |
| 5 mins | 2026-09-13 22:29:07.759Z | 345.557° N | 2026-09-13 22:31:07.759Z | 269.207° W | 44.872° | 2026-09-13 22:34:07.759Z | 212.889° SW |
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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