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 00053U 26101.49828578 +.00000000 +00000-0 -61572-3 0 00007
2 00053 47.2766 188.0513 0100782 238.1647 120.9299 12.17409210 06
| Epoch (UTC): | 11 April 2026 11:57:31 |
| Eccentricity: | 0.0100782 |
| inclination: | 47.2766° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 188.0513° |
| argument of perigee: | 238.1647° |
| revolutions per day: | 12.17409210 |
| mean anomaly at epoch: | 120.9299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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