R5-S4, 60206
Orbit data source: Space-Track
R5-S4, 60206 is a payload satellite owned by NASA JSC (US) in SSO that was launched on Thu, 04 Jul 2024 UTC via an FIREFLY ALPHA 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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60206 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NASA JSC
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 R5-S4
1 60206U 24125D 25303.55864438 .00019771 00000-0 57589-3 0 9996
2 60206 97.2630 152.0292 0019153 345.4971 14.5721 15.35246292 73803Epoch: 2025-10-30T13:24Z
TLE epoch observation values (Epoch: 2025-10-30T13:24:26.874Z)
Latitude
0.00002°
Longitude
-88.19848°
Altitude
450.627 km
Speed
7.649 km/s
True Right ascension
10h 08m 07s
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
01:29:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.22 km
Perigee altitude
444.037 km
Semi-major axis
6,835.265 km
Eccentricity
0.00192
Inclination
97.263°
RAAN
152.0292°
Arg. of periapsis
345.4971°
True anomaly
14.62745°
Mean anomaly
14.5721°
Eccentric anomaly
14.59976°
Mean motion
3.8407 °/min
Orbital period
93.73 mins
BSTAR
0.00057589
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Other satellites on launch #125 in the year 2024 (2024-07-04 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.R5-S4 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 | 2025-10-31 14:34:40.949Z | 212.357° SW | 2025-10-31 14:36:40.949Z | 276.302° WNW | 28.069° | 2025-10-31 14:38:40.949Z | 321.909° NNW |
| 4 mins | 2025-11-01 03:31:40.949Z | 322.243° NNW | 2025-11-01 03:32:40.949Z | 294.359° NW | 24.751° | 2025-11-01 03:35:40.949Z | 230.226° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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