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 59588U 26099.80287108 +.00000000 +00000-0 +16853-1 0 00002
2 59588 97.1912 33.9249 0073068 8.5394 351.6995 13.91125721 09
| Epoch (UTC): | 09 April 2026 19:16:08 |
| Eccentricity: | 0.0073068 |
| inclination: | 97.1912° |
| perigee height: | 871 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 33.9249° |
| argument of perigee: | 8.5394° |
| revolutions per day: | 13.91125721 |
| mean anomaly at epoch: | 351.6995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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