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 28521U 26106.89886181 +.00000000 +00000-0 +18898-4 0 00003
2 28521 82.9462 90.0050 0040963 142.4450 217.9587 13.87919603 03
| Epoch (UTC): | 16 April 2026 21:34:21 |
| Eccentricity: | 0.0040963 |
| inclination: | 82.9462° |
| perigee height: | 906 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 90.0050° |
| argument of perigee: | 142.4450° |
| revolutions per day: | 13.87919603 |
| mean anomaly at epoch: | 217.9587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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