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 24753U 26140.56681660 +.00000000 +00000-0 +52065-4 0 00007
2 24753 98.7597 189.5540 0009092 163.4242 196.7231 14.16763464 03
| Epoch (UTC): | 20 May 2026 13:36:12 |
| Eccentricity: | 0.0009092 |
| inclination: | 98.7597° |
| perigee height: | 830 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 189.5540° |
| argument of perigee: | 163.4242° |
| revolutions per day: | 14.16763464 |
| mean anomaly at epoch: | 196.7231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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