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 62166U 26145.24247940 +.00000000 +00000-0 +12730-2 0 00009
2 62166 70.0023 331.3748 0002665 262.0225 98.0632 14.98355893 05
| Epoch (UTC): | 25 May 2026 05:49:10 |
| Eccentricity: | 0.0002665 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.3748° |
| argument of perigee: | 262.0225° |
| revolutions per day: | 14.98355893 |
| mean anomaly at epoch: | 98.0632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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