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 62507U 26145.49759455 +.00000000 +00000-0 +51746-3 0 00005
2 62507 43.0002 215.5635 0001659 275.6769 84.3893 15.27589693 01
| Epoch (UTC): | 25 May 2026 11:56:32 |
| Eccentricity: | 0.0001659 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.5635° |
| argument of perigee: | 275.6769° |
| revolutions per day: | 15.27589693 |
| mean anomaly at epoch: | 84.3893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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