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 26072.98510266 +.00000000 +00000-0 +71679-4 0 00004
2 24773 82.9250 167.2708 0025462 65.1972 108.0626 13.73972795 07
| Epoch (UTC): | 13 March 2026 23:38:32 |
| Eccentricity: | 0.0025462 |
| inclination: | 82.9250° |
| perigee height: | 967 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 167.2708° |
| argument of perigee: | 65.1972° |
| revolutions per day: | 13.73972795 |
| mean anomaly at epoch: | 108.0626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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