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 13068U 26072.92206972 +.00000000 +00000-0 +20776-3 0 00000
2 13068 81.1758 155.8105 0022855 163.1775 197.0221 15.22060968 08
| Epoch (UTC): | 13 March 2026 22:07:46 |
| Eccentricity: | 0.0022855 |
| inclination: | 81.1758° |
| perigee height: | 484 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 155.8105° |
| argument of perigee: | 163.1775° |
| revolutions per day: | 15.22060968 |
| mean anomaly at epoch: | 197.0221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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