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
7.44 kg wet, 7 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: 1 day ago
TLE from 1 day ago
0 R5-S4
1 60206U 24125D 25348.57156559 .00013657 00000-0 37644-3 0 9992
2 60206 97.2573 196.4335 0018445 173.6091 186.5392 15.37062994 80715Epoch: 2025-12-14T13:43Z
TLE epoch observation values (Epoch: 2025-12-14T13:43:03.266Z)
Latitude
-0.00012°
Longitude
-92.81266°
Altitude
470.442 km
Speed
7.624 km/s
True Right ascension
13h 05m 44s
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
13:22:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.334 km
Perigee altitude
439.139 km
Semi-major axis
6,829.873 km
Eccentricity
0.00184
Inclination
97.2573°
RAAN
196.4335°
Arg. of periapsis
173.6091°
True anomaly
186.51518°
Mean anomaly
186.5392°
Eccentric anomaly
186.52719°
Mean motion
3.84525 °/min
Orbital period
93.62 mins
BSTAR
0.00037644
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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 | 2025-12-15 14:51:21.868Z | 226.12° WSW | 2025-12-15 14:53:21.868Z | 270.779° WNW | 19.273° | 2025-12-15 14:55:21.868Z | 310.333° NW |
| 4 mins | 2025-12-16 02:14:21.868Z | 58.569° ENE | 2025-12-16 02:16:21.868Z | 109.682° ESE | 20.257° | 2025-12-16 02:18:21.868Z | 147.642° SSE |
| 5 mins | 2025-12-16 14:17:21.868Z | 183.993° SSW | 2025-12-16 14:19:21.868Z | 244.359° WSW | 40.655° | 2025-12-16 14:22:21.868Z | 338.825° 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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