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 24907U 26088.16934919 +.00000000 +00000-0 +12418-3 0 00000
2 24907 86.4019 354.6269 0002208 90.1420 270.0030 14.36211703 05
| Epoch (UTC): | 29 March 2026 04:03:51 |
| Eccentricity: | 0.0002208 |
| inclination: | 86.4019° |
| perigee height: | 769 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 354.6269° |
| argument of perigee: | 90.1420° |
| revolutions per day: | 14.36211703 |
| mean anomaly at epoch: | 270.0030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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