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 53105U 26142.50022807 +.00000000 +00000-0 +00000-0 0 00006
2 53105 70.1680 314.1386 0005374 340.7508 19.2827 6.38965148 09
| Epoch (UTC): | 22 May 2026 12:00:19 |
| Eccentricity: | 0.0005374 |
| inclination: | 70.1680° |
| perigee height: | 5883 km |
| apogee height: | 5896 km |
| right ascension of ascending node: | 314.1386° |
| argument of perigee: | 340.7508° |
| revolutions per day: | 6.38965148 |
| mean anomaly at epoch: | 19.2827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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