Showing default

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.

Loading next visibility...
Identifier
60206, 2024-125D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
NASA JSC
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
2024-07-04 (1 year ago)
Launch vehicle
FIREFLY ALPHA
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 R5-S4
1 60206U 24125D   25258.55948849  .00009886  00000-0  30546-3 0  9994
2 60206  97.2711 107.7182 0021452 138.1341 222.1548 15.33495697 66901
Epoch: 2025-09-15T13:25Z
TLE epoch observation values (Epoch: 2025-09-15T13:25:39.805Z)
Latitude
0.00005°
Longitude
-88.46006°
Altitude
479.405 km
Speed
7.62 km/s
True Right ascension
07h 10m 52s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:47:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.009 km
Perigee altitude
447.66 km
Semi-major axis
6,840.471 km
Eccentricity
0.00215
Inclination
97.2711°
RAAN
107.7182°
Arg. of periapsis
138.1341°
True anomaly
221.99015°
Mean anomaly
222.1548°
Eccentric anomaly
222.07244°
Mean motion
3.83631 °/min
Orbital period
93.84 mins
BSTAR
0.00030546
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|