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 58941U 26144.86373551 +.00000000 +00000-0 +18166-4 0 00001
2 58941 53.1614 315.6086 0001191 91.8078 268.3059 15.30190985 07
| Epoch (UTC): | 24 May 2026 20:43:46 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 315.6086° |
| argument of perigee: | 91.8078° |
| revolutions per day: | 15.30190985 |
| mean anomaly at epoch: | 268.3059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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