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 05679U 26088.16601015 +.00000000 +00000-0 +71007-4 0 00003
2 05679 69.9970 167.5476 0014935 229.8637 130.1155 13.85676628 02
| Epoch (UTC): | 29 March 2026 03:59:03 |
| Eccentricity: | 0.0014935 |
| inclination: | 69.9970° |
| perigee height: | 933 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 167.5476° |
| argument of perigee: | 229.8637° |
| revolutions per day: | 13.85676628 |
| mean anomaly at epoch: | 130.1155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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