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 45660U 26145.48318000 +.00000000 +00000-0 +13003-2 0 00005
2 45660 53.1335 68.9689 0004333 60.9020 299.2414 15.31179002 09
| Epoch (UTC): | 25 May 2026 11:35:46 |
| Eccentricity: | 0.0004333 |
| inclination: | 53.1335° |
| perigee height: | 469 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 68.9689° |
| argument of perigee: | 60.9020° |
| revolutions per day: | 15.31179002 |
| mean anomaly at epoch: | 299.2414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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