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 62973U 26145.52268536 +.00000000 +00000-0 +21975-4 0 00003
2 62973 50.0046 317.1099 0001091 95.6468 264.4529 13.29326861 06
| Epoch (UTC): | 25 May 2026 12:32:40 |
| Eccentricity: | 0.0001091 |
| inclination: | 50.0046° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 317.1099° |
| argument of perigee: | 95.6468° |
| revolutions per day: | 13.29326861 |
| mean anomaly at epoch: | 264.4529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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