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 43178U 18013A 25359.60185783 0.00000000 00000-0 00000-0 0 01
2 43178 0.0302 332.4572 0004000 266.3572 93.6428 1.00270000 03
| Epoch (UTC): | 25 December 2025 14:26:40 |
| Eccentricity: | 0.0004000 |
| inclination: | 0.0302° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 332.4572° |
| argument of perigee: | 266.3572° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 93.6428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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