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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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Identifier
60206, 2024-125D
Orbit
SSO
Last TLE update
10 hours ago
Origin
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

TLE from 10 hours ago
0 R5-S4
1 60206U 24125D   25199.54348018  .00007837  00000-0  25350-3 0  9990
2 60206  97.2787  49.6846 0020646 357.5228   2.5909 15.32126038 57865
Epoch: 2025-07-18T13:02Z
TLE epoch observation values (Epoch: 2025-07-18T13:02:36.687Z)
Latitude
0.00004°
Longitude
-82.5617°
Altitude
458.454 km
Speed
7.645 km/s
True Right ascension
03h 18m 44s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
47.23565°
Longitude
105.741°
Altitude
487.062 km
Speed
7.621 km/s
Apparent Right ascension
19h 59m 49s
Apparent Declination
11° 03' 29"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
11:48:56
Azimuth
59.442° ENE
Elevation
-16.487°
Doppler factor
1
Orbital elements
Apogee altitude
480.546 km
Perigee altitude
452.283 km
Semi-major axis
6,844.552 km
Eccentricity
0.00206
Inclination
97.2787°
RAAN
49.6846°
Arg. of periapsis
357.5228°
True anomaly
2.60162°
Mean anomaly
2.5909°
Eccentric anomaly
2.59626°
Mean motion
3.83288 °/min
Orbital period
93.92 mins
BSTAR
0.0002535
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