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 48143U 26145.10205009 +.00000000 +00000-0 +12637-2 0 00009
2 48143 53.1567 104.3635 0005858 46.4014 313.7475 15.36939831 04
| Epoch (UTC): | 25 May 2026 02:26:57 |
| Eccentricity: | 0.0005858 |
| inclination: | 53.1567° |
| perigee height: | 451 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 104.3635° |
| argument of perigee: | 46.4014° |
| revolutions per day: | 15.36939831 |
| mean anomaly at epoch: | 313.7475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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