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 Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
7.44 kg wet, 7 kg dry
Launch date (UTC)
2024-07-04 (2 years ago)
Launch vehicle
FIREFLY ALPHA
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.9 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 R5-S4
1 60206U 24125D   26266.95184964  .00013156  00000-0  27273-3 0  9996
2 60206  97.2267 117.7022 0013876 226.2619 133.7483 15.45754516124371
Epoch: 2026-09-23T22:50Z
TLE epoch observation values (Epoch: 2026-09-23T22:50:39.808Z)
Latitude
-0.00001°
Longitude
132.24073°
Altitude
438.832 km
Speed
7.645 km/s
True Right ascension
07h 50m 48s
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
04:32:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.527 km
Perigee altitude
416.644 km
Semi-major axis
6,804.223 km
Eccentricity
0.00139
Inclination
97.2267°
RAAN
117.7022°
Arg. of periapsis
226.2619°
True anomaly
133.86303°
Mean anomaly
133.7483°
Eccentric anomaly
133.80568°
Mean motion
3.86701 °/min
Orbital period
93.1 mins
BSTAR
0.00027273
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
|