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 62491U 26145.58725404 +.00000000 +00000-0 +46092-3 0 00002
2 62491 43.0025 214.5627 0002185 259.9885 100.0721 15.27586033 08
| Epoch (UTC): | 25 May 2026 14:05:38 |
| Eccentricity: | 0.0002185 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 214.5627° |
| argument of perigee: | 259.9885° |
| revolutions per day: | 15.27586033 |
| mean anomaly at epoch: | 100.0721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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