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 55571U 26145.45797551 +.00000000 +00000-0 +21116-3 0 00001
2 55571 43.0105 295.0538 0002402 268.6372 91.4205 15.27605366 04
| Epoch (UTC): | 25 May 2026 10:59:29 |
| Eccentricity: | 0.0002402 |
| inclination: | 43.0105° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 295.0538° |
| argument of perigee: | 268.6372° |
| revolutions per day: | 15.27605366 |
| mean anomaly at epoch: | 91.4205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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