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 05917U 26157.12571617 +.00000000 +00000-0 +15427-3 0 00008
2 05917 81.2297 295.9646 0050216 5.2841 354.8848 14.09278873 07
| Epoch (UTC): | 06 June 2026 03:01:01 |
| Eccentricity: | 0.0050216 |
| inclination: | 81.2297° |
| perigee height: | 825 km |
| apogee height: | 898 km |
| right ascension of ascending node: | 295.9646° |
| argument of perigee: | 5.2841° |
| revolutions per day: | 14.09278873 |
| mean anomaly at epoch: | 354.8848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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