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 58072U 26145.48915022 +.00000000 +00000-0 +89007-4 0 00002
2 58072 42.9998 313.4699 0001136 270.7840 89.2881 15.27579813 03
| Epoch (UTC): | 25 May 2026 11:44:22 |
| Eccentricity: | 0.0001136 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.4699° |
| argument of perigee: | 270.7840° |
| revolutions per day: | 15.27579813 |
| mean anomaly at epoch: | 89.2881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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