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 26100.11396080 +.00000000 +00000-0 +68152-5 0 00009
2 05917 81.2311 351.4970 0048264 163.7811 196.4918 14.09259388 07
| Epoch (UTC): | 10 April 2026 02:44:06 |
| Eccentricity: | 0.0048264 |
| inclination: | 81.2311° |
| perigee height: | 827 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 351.4970° |
| argument of perigee: | 163.7811° |
| revolutions per day: | 14.09259388 |
| mean anomaly at epoch: | 196.4918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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