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 57843U 26144.81769568 +.00000000 +00000-0 +22448-4 0 00001
2 57843 53.1613 290.3017 0001158 84.2575 275.8558 15.31700391 06
| Epoch (UTC): | 24 May 2026 19:37:28 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 290.3017° |
| argument of perigee: | 84.2575° |
| revolutions per day: | 15.31700391 |
| mean anomaly at epoch: | 275.8558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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