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 62275U 26145.48866332 +.00000000 +00000-0 +18125-2 0 00002
2 62275 42.9979 314.3259 0002229 277.5458 82.5156 15.70913767 07
| Epoch (UTC): | 25 May 2026 11:43:40 |
| Eccentricity: | 0.0002229 |
| inclination: | 42.9979° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 314.3259° |
| argument of perigee: | 277.5458° |
| revolutions per day: | 15.70913767 |
| mean anomaly at epoch: | 82.5156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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