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 12849U 26088.12385933 +.00000000 +00000-0 +10724-3 0 00002
2 12849 82.4883 217.0889 0869763 43.0700 323.5252 13.58140323 09
| Epoch (UTC): | 29 March 2026 02:58:21 |
| Eccentricity: | 0.0869763 |
| inclination: | 82.4883° |
| perigee height: | 397 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 217.0889° |
| argument of perigee: | 43.0700° |
| revolutions per day: | 13.58140323 |
| mean anomaly at epoch: | 323.5252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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