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 24278U 26066.57661174 +.00000000 +00000-0 +20951-4 0 00004
2 24278 98.5383 289.2820 0349916 0.2496 359.8759 13.53268594 07
| Epoch (UTC): | 07 March 2026 13:50:19 |
| Eccentricity: | 0.0349916 |
| inclination: | 98.5383° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 289.2820° |
| argument of perigee: | 0.2496° |
| revolutions per day: | 13.53268594 |
| mean anomaly at epoch: | 359.8759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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