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 24773U 26161.61085697 +.00000000 +00000-0 +26202-4 0 00000
2 24773 82.9209 101.5404 0024270 173.0921 4.4531 13.73977636 07
| Epoch (UTC): | 10 June 2026 14:39:38 |
| Eccentricity: | 0.0024270 |
| inclination: | 82.9209° |
| perigee height: | 967 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 101.5404° |
| argument of perigee: | 173.0921° |
| revolutions per day: | 13.73977636 |
| mean anomaly at epoch: | 4.4531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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