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 54059U 26145.33191740 +.00000000 +00000-0 +22989-3 0 00005
2 54059 53.2152 0.1087 0001357 96.5270 263.5877 15.08824028 00
| Epoch (UTC): | 25 May 2026 07:57:57 |
| Eccentricity: | 0.0001357 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 0.1087° |
| argument of perigee: | 96.5270° |
| revolutions per day: | 15.08824028 |
| mean anomaly at epoch: | 263.5877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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