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 58100U 26145.45110547 +.00000000 +00000-0 +78996-5 0 00006
2 58100 53.1594 169.0089 0001172 83.9036 276.2099 15.30189846 06
| Epoch (UTC): | 25 May 2026 10:49:35 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0089° |
| argument of perigee: | 83.9036° |
| revolutions per day: | 15.30189846 |
| mean anomaly at epoch: | 276.2099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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