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). Payloads include a variety of satellites, spacecraft, and rockets 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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R5-S4 radio frequencies
R5-S4 details
Identifier | |
Orbit | SSO |
Last TLE update | 1 day ago |
Origin | |
Manufacturer | NASA JSC |
Mission | Operational spacecraft |
Bus & Motor | CUBESAT 6U, Unknown motor |
Mass | 10 kg wet, ~10 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 R5-S4
1 60206U 24125D 24355.58310871 .00012636 00000-0 49412-3 0 9991
2 60206 97.2980 203.8888 0025042 22.8705 337.3643 15.25686614 25779
Epoch: 2024-12-20T13:59Z
Definitive object data (Epoch: 2024-12-20T13:59:40.592Z)
Latitude | -0.00001° |
Longitude | -95.67687° |
Altitude | 475.957 km |
Speed | 7.637 km/s |
True Right ascension | 13h 35m 33s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 69.99128° |
Longitude | 105.8389° |
Altitude | 500.623 km |
Speed | 7.621 km/s |
Apparent Right ascension | 02h 48m 02s |
Apparent Declination | 18° 05' 53" |
Sunlit | Object is in full shadow |
Visualization observer readout
Local Sidereal Time | 14:41:30 |
Azimuth | 358.168° N |
Elevation | -31.966° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 502.866 km |
Perigee altitude | 468.49 km |
Semi-major axis | 6,863.815 km |
Eccentricity | 0.0025042 |
Inclination | 97.298° |
RAAN | 203.8888° |
Arg. of periapsis | 22.8705° |
True anomaly | 337.25354° |
Mean anomaly | 337.3643° |
Eccentric anomaly | 337.30895° |
Mean motion | 3.81676 °/min |
BSTAR | 0.00049412 |
Orbital period | 94.32 mins |
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Other satellites on launch #125 in the year 2024 (2024-07-04 UTC)
OBJECT A, 60203 |
OBJECT B, 60204 |
OBJECT C, 60205 |
R5-S4, 60206 |
R5-S2, 60207 |
TECHEDSAT-11, 60208 |
OBJECT G, 60209 |
FIREFLY ALPHA R/B, 60210 |
CATSAT, 60246 |
R5-S4 Visibility forecast
Observer location: undefined°, undefined
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. |
---|---|---|---|---|---|---|---|
6 mins | 2024-12-22 02:45:10.393Z | 20.661° NNE | 2024-12-22 02:48:10.393Z | 72.078° E | 39.245° | 2024-12-22 02:51:10.393Z | 176.684° S |
4 mins | 2024-12-22 14:56:10.393Z | 232.632° WSW | 2024-12-22 14:57:10.393Z | 255.13° W | 19.715° | 2024-12-22 15:00:10.393Z | 315.338° NNW |
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