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 40973U 26145.51994483 +.00000000 +00000-0 +30084-3 0 00005
2 40973 64.7693 323.3487 0123269 68.9714 292.4532 14.94086429 02
| Epoch (UTC): | 25 May 2026 12:28:43 |
| Eccentricity: | 0.0123269 |
| inclination: | 64.7693° |
| perigee height: | 499 km |
| apogee height: | 671 km |
| right ascension of ascending node: | 323.3487° |
| argument of perigee: | 68.9714° |
| revolutions per day: | 14.94086429 |
| mean anomaly at epoch: | 292.4532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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