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 53779U 26145.38988321 +.00000000 +00000-0 -80392-4 0 00001
2 53779 53.2152 289.9161 0000900 101.0251 259.0842 15.08828976 00
| Epoch (UTC): | 25 May 2026 09:21:25 |
| Eccentricity: | 0.0000900 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 289.9161° |
| argument of perigee: | 101.0251° |
| revolutions per day: | 15.08828976 |
| mean anomaly at epoch: | 259.0842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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