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 20478U 26088.14715509 +.00000000 +00000-0 +64814-4 0 00007
2 20478 99.2267 149.1530 0006052 52.7577 307.4136 13.96052628 03
| Epoch (UTC): | 29 March 2026 03:31:54 |
| Eccentricity: | 0.0006052 |
| inclination: | 99.2267° |
| perigee height: | 903 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 149.1530° |
| argument of perigee: | 52.7577° |
| revolutions per day: | 13.96052628 |
| mean anomaly at epoch: | 307.4136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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