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 62880U 26145.52668854 +.00000000 +00000-0 +12590-2 0 00008
2 62880 43.0014 78.0786 0000958 290.2243 69.8522 15.70887525 08
| Epoch (UTC): | 25 May 2026 12:38:25 |
| Eccentricity: | 0.0000958 |
| inclination: | 43.0014° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 78.0786° |
| argument of perigee: | 290.2243° |
| revolutions per day: | 15.70887525 |
| mean anomaly at epoch: | 69.8522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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