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 05730U 26108.93139285 +.00000000 +00000-0 +41415-3 0 00003
2 05730 73.8839 100.4539 0545547 58.5659 306.7649 14.38535864 07
| Epoch (UTC): | 18 April 2026 22:21:12 |
| Eccentricity: | 0.0545547 |
| inclination: | 73.8839° |
| perigee height: | 374 km |
| apogee height: | 1153 km |
| right ascension of ascending node: | 100.4539° |
| argument of perigee: | 58.5659° |
| revolutions per day: | 14.38535864 |
| mean anomaly at epoch: | 306.7649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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