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 31127U 26145.40308475 +.00000000 +00000-0 +11192-3 0 00003
2 31127 98.3971 117.5114 0062774 330.7230 29.0459 14.64481601 01
| Epoch (UTC): | 25 May 2026 09:40:26 |
| Eccentricity: | 0.0062774 |
| inclination: | 98.3971° |
| perigee height: | 634 km |
| apogee height: | 723 km |
| right ascension of ascending node: | 117.5114° |
| argument of perigee: | 330.7230° |
| revolutions per day: | 14.64481601 |
| mean anomaly at epoch: | 29.0459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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