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 12646U 26088.20662875 +.00000000 +00000-0 +48417-4 0 00000
2 12646 81.2299 352.7059 0066695 188.3830 282.8642 14.16416240 07
| Epoch (UTC): | 29 March 2026 04:57:32 |
| Eccentricity: | 0.0066695 |
| inclination: | 81.2299° |
| perigee height: | 789 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 352.7059° |
| argument of perigee: | 188.3830° |
| revolutions per day: | 14.16416240 |
| mean anomaly at epoch: | 282.8642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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