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 26145.46771132 +.00000000 +00000-0 +42061-4 0 00007
2 28521 82.9509 60.8306 0041058 35.8169 324.5734 13.87924157 01
| Epoch (UTC): | 25 May 2026 11:13:30 |
| Eccentricity: | 0.0041058 |
| inclination: | 82.9509° |
| perigee height: | 906 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 60.8306° |
| argument of perigee: | 35.8169° |
| revolutions per day: | 13.87924157 |
| mean anomaly at epoch: | 324.5734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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