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 24834U 26104.07903652 +.00000000 +00000-0 +00000-0 0 00009
2 24834 15.6220 6.5488 0104191 237.1336 310.1917 0.96051622 04
| Epoch (UTC): | 14 April 2026 01:53:48 |
| Eccentricity: | 0.0104191 |
| inclination: | 15.6220° |
| perigee height: | 36561 km |
| apogee height: | 37465 km |
| right ascension of ascending node: | 6.5488° |
| argument of perigee: | 237.1336° |
| revolutions per day: | 0.96051622 |
| mean anomaly at epoch: | 310.1917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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