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 66521U 26145.52452137 +.00000000 +00000-0 +43375-3 0 00005
2 66521 42.9992 204.0733 0001490 275.1356 84.9326 15.27588444 09
| Epoch (UTC): | 25 May 2026 12:35:18 |
| Eccentricity: | 0.0001490 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.0733° |
| argument of perigee: | 275.1356° |
| revolutions per day: | 15.27588444 |
| mean anomaly at epoch: | 84.9326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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