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). 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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60207 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | SSO |
| Last TLE update | 5 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) | |
| 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 5 hours ago
0 R5-S2
1 60207U 24125E 25082.57017408 .00024101 00000-0 83155-3 0 9991
2 60207 97.2915 294.9286 0023375 53.7008 306.6387 15.29704178 39978Epoch: 2025-03-23T13:41Z
Definitive object data (Epoch: 2025-03-23T13:41:03.04Z)
| Latitude | -0° |
| Longitude | -91.63306° |
| Altitude | 470.263 km |
| Speed | 7.636 km/s |
| True Right ascension | 19h 39m 42s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -22.67716° |
| Longitude | -88.39685° |
| Altitude | 481.32 km |
| Speed | 7.626 km/s |
| Apparent Right ascension | 16h 35m 48s |
| Apparent Declination | -52° 29' 49" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 23:23:10 |
| Azimuth | 228.439° WSW |
| Elevation | -37.221° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 489.66 km |
| Perigee altitude | 457.628 km |
| Semi-major axis | 6,851.781 km |
| Eccentricity | 0.0023375 |
| Inclination | 97.2915° |
| RAAN | 294.9286° |
| Arg. of periapsis | 53.7008° |
| True anomaly | 306.42339° |
| Mean anomaly | 306.6387° |
| Eccentric anomaly | 306.53108° |
| Mean motion | 3.82682 °/min |
| BSTAR | 0.00083155 |
| Orbital period | 94.07 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 |
| TECHEDSAT-11, 60208 |
| OBJECT G, 60209 |
| FIREFLY ALPHA R/B, 60210 |
| CATSAT, 60246 |
R5-S2 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 | 2025-03-24 02:47:41.935Z | 17.227° NNE | 2025-03-24 02:50:41.935Z | 57.113° ENE | 41.102° | 2025-03-24 02:53:41.935Z | 182.447° SSW |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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