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 62188U 26097.11654698 +.00000000 +00000-0 +00000-0 0 00002
2 62188 63.7291 47.3208 7016081 269.4800 17.0700 2.00644402 08
| Epoch (UTC): | 07 April 2026 02:47:49 |
| Eccentricity: | 0.7016081 |
| inclination: | 63.7291° |
| perigee height: | 1545 km |
| apogee height: | 38805 km |
| right ascension of ascending node: | 47.3208° |
| argument of perigee: | 269.4800° |
| revolutions per day: | 2.00644402 |
| mean anomaly at epoch: | 17.0700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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