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 58698U 26145.59560182 +.00000000 +00000-0 +00000-0 0 00003
2 58698 0.0114 245.0031 0000090 157.4810 114.7829 1.00272380 09
| Epoch (UTC): | 25 May 2026 14:17:39 |
| Eccentricity: | 0.0000090 |
| inclination: | 0.0114° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 245.0031° |
| argument of perigee: | 157.4810° |
| revolutions per day: | 1.00272380 |
| mean anomaly at epoch: | 114.7829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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