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 39497U 26097.21452742 +.00000000 +00000-0 +12166-3 0 00005
2 39497 82.4879 212.4746 0012358 241.9780 118.0050 12.43495839 01
| Epoch (UTC): | 07 April 2026 05:08:55 |
| Eccentricity: | 0.0012358 |
| inclination: | 82.4879° |
| perigee height: | 1482 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 212.4746° |
| argument of perigee: | 241.9780° |
| revolutions per day: | 12.43495839 |
| mean anomaly at epoch: | 118.0050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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