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 21575U 26106.92209787 +.00000000 +00000-0 +47042-4 0 00003
2 21575 98.3536 176.6690 0007176 10.2290 349.9045 14.42345884 03
| Epoch (UTC): | 16 April 2026 22:07:49 |
| Eccentricity: | 0.0007176 |
| inclination: | 98.3536° |
| perigee height: | 746 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 176.6690° |
| argument of perigee: | 10.2290° |
| revolutions per day: | 14.42345884 |
| mean anomaly at epoch: | 349.9045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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