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 12650U 26101.27526933 +.00000000 +00000-0 +39086-3 0 00003
2 12650 82.9318 281.6093 0063403 15.0406 158.7061 13.80965177 03
| Epoch (UTC): | 11 April 2026 06:36:23 |
| Eccentricity: | 0.0063403 |
| inclination: | 82.9318° |
| perigee height: | 914 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 281.6093° |
| argument of perigee: | 15.0406° |
| revolutions per day: | 13.80965177 |
| mean anomaly at epoch: | 158.7061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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