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 58426U 26145.64424500 +.00000000 +00000-0 +11361-3 0 00006
2 58426 49.9598 49.4418 0010892 202.4636 157.5766 13.41488566 07
| Epoch (UTC): | 25 May 2026 15:27:42 |
| Eccentricity: | 0.0010892 |
| inclination: | 49.9598° |
| perigee height: | 1096 km |
| apogee height: | 1112 km |
| right ascension of ascending node: | 49.4418° |
| argument of perigee: | 202.4636° |
| revolutions per day: | 13.41488566 |
| mean anomaly at epoch: | 157.5766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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