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 58118U 26145.46565360 +.00000000 +00000-0 -16204-4 0 00007
2 58118 43.0050 58.5074 0000989 256.9114 103.1627 15.27576899 09
| Epoch (UTC): | 25 May 2026 11:10:32 |
| Eccentricity: | 0.0000989 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.5074° |
| argument of perigee: | 256.9114° |
| revolutions per day: | 15.27576899 |
| mean anomaly at epoch: | 103.1627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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