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 57902U 26145.32128866 +.00000000 +00000-0 -26874-4 0 00002
2 57902 43.0043 241.6357 0001907 287.8842 72.1802 15.27561543 02
| Epoch (UTC): | 25 May 2026 07:42:39 |
| Eccentricity: | 0.0001907 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 241.6357° |
| argument of perigee: | 287.8842° |
| revolutions per day: | 15.27561543 |
| mean anomaly at epoch: | 72.1802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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