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 20608U 26088.16298259 +.00000000 +00000-0 +20173-3 0 00001
2 20608 89.7447 247.6965 0084174 96.3803 264.7015 14.80559462 08
| Epoch (UTC): | 29 March 2026 03:54:41 |
| Eccentricity: | 0.0084174 |
| inclination: | 89.7447° |
| perigee height: | 569 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 247.6965° |
| argument of perigee: | 96.3803° |
| revolutions per day: | 14.80559462 |
| mean anomaly at epoch: | 264.7015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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