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 26145.16733686 +.00000000 +00000-0 -13592-4 0 00008
2 39497 82.4855 182.5801 0014096 137.3899 222.8277 12.43496672 05
| Epoch (UTC): | 25 May 2026 04:00:57 |
| Eccentricity: | 0.0014096 |
| inclination: | 82.4855° |
| perigee height: | 1481 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 182.5801° |
| argument of perigee: | 137.3899° |
| revolutions per day: | 12.43496672 |
| mean anomaly at epoch: | 222.8277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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