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 62885U 26145.51607690 +.00000000 +00000-0 +16191-2 0 00004
2 62885 43.0023 77.9897 0001132 42.5149 317.5807 15.70886762 03
| Epoch (UTC): | 25 May 2026 12:23:09 |
| Eccentricity: | 0.0001132 |
| inclination: | 43.0023° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 77.9897° |
| argument of perigee: | 42.5149° |
| revolutions per day: | 15.70886762 |
| mean anomaly at epoch: | 317.5807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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