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: 6 hours ago
TLE from 6 hours ago
0 LIZZIESAT
1 59132U 24043AL 26059.25670576 .00004679 00000-0 18191-3 0 9992
2 59132 97.5442 193.7428 0009576 268.1299 91.8843 15.26509627110313Epoch: 2026-02-28T06:09Z
TLE epoch observation values (Epoch: 2026-02-28T06:09:39.377Z)
Latitude
0.00001°
Longitude
-56.7527°
Altitude
489.574 km
Speed
7.62 km/s
True Right ascension
12h 54m 58s
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
15:21:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.79 km
Perigee altitude
476.649 km
Semi-major axis
6,861.356 km
Eccentricity
0.00096
Inclination
97.5442°
RAAN
193.7428°
Arg. of periapsis
268.1299°
True anomaly
91.99397°
Mean anomaly
91.8843°
Eccentric anomaly
91.93914°
Mean motion
3.81881 °/min
Orbital period
94.27 mins
BSTAR
0.00018191
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-28 20:54:13.649Z | 56.392° ENE | 2026-02-28 20:56:13.649Z | 94.417° ESE | 17.161° | 2026-02-28 20:58:13.649Z | 132.461° SE |
| 4 mins | 2026-02-28 22:28:13.649Z | 325.035° NNW | 2026-02-28 22:29:13.649Z | 301.531° NW | 22.5° | 2026-02-28 22:32:13.649Z | 237.03° WSW |
| 5 mins | 2026-03-01 09:03:13.649Z | 180.363° SSW | 2026-03-01 09:05:13.649Z | 308.688° NW | 41.731° | 2026-03-01 09:08:13.649Z | 343.375° N |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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