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 25544U 26134.19858747 +.00000000 +00000-0 +10032-3 0 00007
2 25544 51.6312 108.3512 0007536 56.9254 303.2457 15.49211692 06
| Epoch (UTC): | 14 May 2026 04:45:57 |
| Eccentricity: | 0.0007536 |
| inclination: | 51.6312° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 108.3512° |
| argument of perigee: | 56.9254° |
| revolutions per day: | 15.49211692 |
| mean anomaly at epoch: | 303.2457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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