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 68360U 26100.48006765 +.00000000 +00000-0 +32440-3 0 00007
2 68360 82.2952 88.5876 0022663 11.4642 348.7139 15.85801729 03
| Epoch (UTC): | 10 April 2026 11:31:17 |
| Eccentricity: | 0.0022663 |
| inclination: | 82.2952° |
| perigee height: | 299 km |
| apogee height: | 329 km |
| right ascension of ascending node: | 88.5876° |
| argument of perigee: | 11.4642° |
| revolutions per day: | 15.85801729 |
| mean anomaly at epoch: | 348.7139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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