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 58945U 26145.34353022 +.00000000 +00000-0 -15127-4 0 00005
2 58945 53.1609 275.1357 0000581 89.0610 271.0457 15.30184952 09
| Epoch (UTC): | 25 May 2026 08:14:41 |
| Eccentricity: | 0.0000581 |
| inclination: | 53.1609° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 275.1357° |
| argument of perigee: | 89.0610° |
| revolutions per day: | 15.30184952 |
| mean anomaly at epoch: | 271.0457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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