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 05681U 26100.10958836 +.00000000 +00000-0 +32314-4 0 00009
2 05681 69.9875 146.3292 0010954 259.6919 100.2940 13.74638652 04
| Epoch (UTC): | 10 April 2026 02:37:48 |
| Eccentricity: | 0.0010954 |
| inclination: | 69.9875° |
| perigee height: | 975 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 146.3292° |
| argument of perigee: | 259.6919° |
| revolutions per day: | 13.74638652 |
| mean anomaly at epoch: | 100.2940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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