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 26106.25003654 +.00000000 +00000-0 +20577-4 0 00006
2 28521 82.9461 90.4959 0040923 144.2623 216.1293 13.87919536 02
| Epoch (UTC): | 16 April 2026 06:00:03 |
| Eccentricity: | 0.0040923 |
| inclination: | 82.9461° |
| perigee height: | 906 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 90.4959° |
| argument of perigee: | 144.2623° |
| revolutions per day: | 13.87919536 |
| mean anomaly at epoch: | 216.1293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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