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 21809U 26135.27074338 +.00000000 +00000-0 +15423-3 0 00002
2 21809 63.2967 245.6889 0899215 74.0393 295.7743 13.56258546 09
| Epoch (UTC): | 15 May 2026 06:29:52 |
| Eccentricity: | 0.0899215 |
| inclination: | 63.2967° |
| perigee height: | 381 km |
| apogee height: | 1717 km |
| right ascension of ascending node: | 245.6889° |
| argument of perigee: | 74.0393° |
| revolutions per day: | 13.56258546 |
| mean anomaly at epoch: | 295.7743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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