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 26074.64754047 +.00000000 +00000-0 +64333-4 0 00005
2 24773 82.9249 166.0385 0025416 60.7616 50.7901 13.73972972 04
| Epoch (UTC): | 15 March 2026 15:32:27 |
| Eccentricity: | 0.0025416 |
| inclination: | 82.9249° |
| perigee height: | 967 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 166.0385° |
| argument of perigee: | 60.7616° |
| revolutions per day: | 13.73972972 |
| mean anomaly at epoch: | 50.7901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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