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 26075.15271095 +.00000000 +00000-0 +63477-4 0 00007
2 24278 98.5372 296.6978 0349549 338.0010 20.6432 13.53269236 02
| Epoch (UTC): | 16 March 2026 03:39:54 |
| Eccentricity: | 0.0349549 |
| inclination: | 98.5372° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 296.6978° |
| argument of perigee: | 338.0010° |
| revolutions per day: | 13.53269236 |
| mean anomaly at epoch: | 20.6432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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