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R5-S2, 60207

Orbit data source: Space-Track

R5-S2, 60207 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
60207, 2024-125E
Orbit
SSO
Last TLE update
11 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
Small (<0.1 m²)

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TLE from 11 hours ago
0 R5-S2
1 60207U 24125E   25199.51832973  .00009142  00000-0  28857-3 0  9992
2 60207  97.2783  49.8414 0020659 358.6598   1.4586 15.32859035 57871
Epoch: 2025-07-18T12:26Z
TLE epoch observation values (Epoch: 2025-07-18T12:26:23.688Z)
Latitude
0.00002°
Longitude
-73.32594°
Altitude
456.258 km
Speed
7.647 km/s
True Right ascension
03h 19m 21s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
7.11045°
Longitude
-73.78286°
Altitude
455.809 km
Speed
7.647 km/s
Apparent Right ascension
02h 01m 19s
Apparent Declination
-16° 40' 49"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:13:52
Azimuth
307.167° NW
Elevation
-57.097°
Doppler factor
1
Orbital elements
Apogee altitude
478.366 km
Perigee altitude
450.095 km
Semi-major axis
6,842.367 km
Eccentricity
0.00207
Inclination
97.2783°
RAAN
49.8414°
Arg. of periapsis
358.6598°
True anomaly
1.46464°
Mean anomaly
1.4586°
Eccentric anomaly
1.46162°
Mean motion
3.83472 °/min
Orbital period
93.88 mins
BSTAR
0.00028857
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