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 26156.83369904 +.00000000 +00000-0 -45598-4 0 00003
2 39497 82.4845 175.3053 0014356 113.5615 246.6974 12.43496980 04
| Epoch (UTC): | 05 June 2026 20:00:31 |
| Eccentricity: | 0.0014356 |
| inclination: | 82.4845° |
| perigee height: | 1481 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 175.3053° |
| argument of perigee: | 113.5615° |
| revolutions per day: | 12.43496980 |
| mean anomaly at epoch: | 246.6974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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