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 06059U 26088.12149154 +.00000000 +00000-0 +62056-4 0 00007
2 06059 74.0546 228.7865 0009929 20.3807 339.7740 14.36511749 09
| Epoch (UTC): | 29 March 2026 02:54:56 |
| Eccentricity: | 0.0009929 |
| inclination: | 74.0546° |
| perigee height: | 763 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 228.7865° |
| argument of perigee: | 20.3807° |
| revolutions per day: | 14.36511749 |
| mean anomaly at epoch: | 339.7740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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