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 26064.67164999 +.00000000 +00000-0 +82026-4 0 00007
2 24773 82.9252 173.4325 0025623 87.1477 28.4271 13.73971397 04
| Epoch (UTC): | 05 March 2026 16:07:10 |
| Eccentricity: | 0.0025623 |
| inclination: | 82.9252° |
| perigee height: | 966 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 173.4325° |
| argument of perigee: | 87.1477° |
| revolutions per day: | 13.73971397 |
| mean anomaly at epoch: | 28.4271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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