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 53637U 26145.53528420 +.00000000 +00000-0 +13386-3 0 00008
2 53637 53.2151 239.3285 0001599 80.9167 279.2006 15.08852276 00
| Epoch (UTC): | 25 May 2026 12:50:48 |
| Eccentricity: | 0.0001599 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.3285° |
| argument of perigee: | 80.9167° |
| revolutions per day: | 15.08852276 |
| mean anomaly at epoch: | 279.2006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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