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 54070U 26145.29875609 +.00000000 +00000-0 +83996-4 0 00002
2 54070 53.2125 359.9041 0001130 87.0393 273.0729 15.08831351 07
| Epoch (UTC): | 25 May 2026 07:10:12 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 359.9041° |
| argument of perigee: | 87.0393° |
| revolutions per day: | 15.08831351 |
| mean anomaly at epoch: | 273.0729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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