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 59588U 26161.74498137 +.00000000 +00000-0 +40259-2 0 00009
2 59588 97.1677 81.9722 0058076 68.4687 292.2657 13.93908092 05
| Epoch (UTC): | 10 June 2026 17:52:46 |
| Eccentricity: | 0.0058076 |
| inclination: | 97.1677° |
| perigee height: | 873 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 81.9722° |
| argument of perigee: | 68.4687° |
| revolutions per day: | 13.93908092 |
| mean anomaly at epoch: | 292.2657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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