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 54058U 26145.32822441 +.00000000 +00000-0 +42135-4 0 00008
2 54058 53.2145 0.0849 0001154 91.4377 268.6747 15.08838376 06
| Epoch (UTC): | 25 May 2026 07:52:38 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 0.0849° |
| argument of perigee: | 91.4377° |
| revolutions per day: | 15.08838376 |
| mean anomaly at epoch: | 268.6747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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