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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 VSP ROSE
1 59124U 24043AC 26235.64309427 .00003586 00000-0 12865-3 0 9994
2 59124 97.5699 13.1482 0010627 17.3678 342.7923 15.29336766137295Epoch: 2026-08-23T15:26Z
TLE epoch observation values (Epoch: 2026-08-23T15:26:03.344Z)
Latitude
-0.00007°
Longitude
169.69807°
Altitude
473.931 km
Speed
7.633 km/s
True Right ascension
00h 52m 35s
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
15:53:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.037 km
Perigee altitude
467.472 km
Semi-major axis
6,852.891 km
Eccentricity
0.00106
Inclination
97.5699°
RAAN
13.1482°
Arg. of periapsis
17.3678°
True anomaly
342.75623°
Mean anomaly
342.7923°
Eccentric anomaly
342.77427°
Mean motion
3.82589 °/min
Orbital period
94.1 mins
BSTAR
0.00012865
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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 | 2026-08-24 08:50:18.436Z | 139.634° SSE | 2026-08-24 08:53:18.436Z | 72.926° E | 30.91° | 2026-08-24 08:56:18.436Z | 6.483° NNE |
| 5 mins | 2026-08-24 21:51:18.436Z | 39.191° NE | 2026-08-24 21:53:18.436Z | 125.903° SE | 35.586° | 2026-08-24 21:56:18.436Z | 176.022° S |
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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