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 13553U 26098.31596918 +.00000000 +00000-0 +43800-4 0 00006
2 13553 82.5647 113.6809 0019780 198.6169 172.3799 14.86694561 02
| Epoch (UTC): | 08 April 2026 07:34:59 |
| Eccentricity: | 0.0019780 |
| inclination: | 82.5647° |
| perigee height: | 594 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 113.6809° |
| argument of perigee: | 198.6169° |
| revolutions per day: | 14.86694561 |
| mean anomaly at epoch: | 172.3799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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