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: 10 hours ago
TLE from 10 hours ago
0 LIZZIESAT
1 59132U 24043AL 26149.36168596 .00003887 00000-0 14799-3 0 9998
2 59132 97.5609 284.9149 0009636 317.3946 42.6544 15.27324058124067Epoch: 2026-05-29T08:40Z
TLE epoch observation values (Epoch: 2026-05-29T08:40:49.666Z)
Latitude
-0.00009°
Longitude
-92.18519°
Altitude
482.05 km
Speed
7.627 km/s
True Right ascension
18h 59m 39s
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
03:46:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.388 km
Perigee altitude
474.169 km
Semi-major axis
6,858.915 km
Eccentricity
0.00096
Inclination
97.5609°
RAAN
284.9149°
Arg. of periapsis
317.3946°
True anomaly
42.72928°
Mean anomaly
42.6544°
Eccentric anomaly
42.69184°
Mean motion
3.82085 °/min
Orbital period
94.22 mins
BSTAR
0.00014799
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-29 21:48:46.662Z | 15.854° NNE | 2026-05-29 21:51:46.662Z | 44.566° NE | 41.798° | 2026-05-29 21:55:46.662Z | 187.739° SSW |
| 4 mins | 2026-05-30 08:25:46.662Z | 104.084° ESE | 2026-05-30 08:26:46.662Z | 78.845° E | 23.006° | 2026-05-30 08:29:46.662Z | 16.312° NNE |
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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