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 62216U 26088.17580395 +.00000000 +00000-0 +28762-4 0 00001
2 62216 67.1467 245.3165 0006731 268.2479 91.7834 13.96674207 08
| Epoch (UTC): | 29 March 2026 04:13:09 |
| Eccentricity: | 0.0006731 |
| inclination: | 67.1467° |
| perigee height: | 900 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 245.3165° |
| argument of perigee: | 268.2479° |
| revolutions per day: | 13.96674207 |
| mean anomaly at epoch: | 91.7834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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