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 57840U 26145.64731020 +.00000000 +00000-0 -71563-4 0 00005
2 57840 53.1612 286.4348 0000830 142.5842 217.5218 15.31702625 04
| Epoch (UTC): | 25 May 2026 15:32:07 |
| Eccentricity: | 0.0000830 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 286.4348° |
| argument of perigee: | 142.5842° |
| revolutions per day: | 15.31702625 |
| mean anomaly at epoch: | 217.5218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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