View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 47508U 26145.52383149 +.00000000 +00000-0 +20900-3 0 00004
2 47508 97.2208 189.3221 0004999 286.1708 73.8985 15.34409013 03
| Epoch (UTC): | 25 May 2026 12:34:19 |
| Eccentricity: | 0.0004999 |
| inclination: | 97.2208° |
| perigee height: | 459 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 189.3221° |
| argument of perigee: | 286.1708° |
| revolutions per day: | 15.34409013 |
| mean anomaly at epoch: | 73.8985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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