VSP ROSE, 59124
Orbit data source: Space-Track
VSP ROSE, 59124 is a payload satellite owned by Aerospacelab (BE) 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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59124 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
BE / BELRelated business
Manufacturer
Aerospacelab
Mission
Operational Commercial Imaging
Bus & Motor
AEROSP, Unknown motor
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.963 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 VSP ROSE
1 59124U 24043AC 25352.33552716 .00004367 00000-0 16888-3 0 9997
2 59124 97.5365 121.4963 0011699 158.3289 201.8447 15.26707608 99372Epoch: 2025-12-18T08:03Z
TLE epoch observation values (Epoch: 2025-12-18T08:03:09.546Z)
Latitude
-0.00001°
Longitude
-86.48598°
Altitude
496.215 km
Speed
7.612 km/s
True Right ascension
08h 05m 59s
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
14:53:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.652 km
Perigee altitude
474.599 km
Semi-major axis
6,860.762 km
Eccentricity
0.00117
Inclination
97.5365°
RAAN
121.4963°
Arg. of periapsis
158.3289°
True anomaly
201.79488°
Mean anomaly
201.8447°
Eccentric anomaly
201.81979°
Mean motion
3.81931 °/min
Orbital period
94.26 mins
BSTAR
0.00016888
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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.VSP ROSE 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 | 2025-12-18 21:11:51.952Z | 30.94° NE | 2025-12-18 21:14:51.952Z | 90.917° ESE | 29.785° | 2025-12-18 21:17:51.952Z | 162.781° S |
| 4 mins | 2025-12-19 09:21:51.952Z | 214.613° SW | 2025-12-19 09:23:51.952Z | 274.431° WNW | 27.88° | 2025-12-19 09:25:51.952Z | 319.359° NNW |
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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