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 26088.16220756 +.00000000 +00000-0 +48318-4 0 00001
2 13553 82.5658 123.1831 0019058 233.9484 186.9651 14.86683533 01
| Epoch (UTC): | 29 March 2026 03:53:34 |
| Eccentricity: | 0.0019058 |
| inclination: | 82.5658° |
| perigee height: | 595 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 123.1831° |
| argument of perigee: | 233.9484° |
| revolutions per day: | 14.86683533 |
| mean anomaly at epoch: | 186.9651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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