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 26131.62401075 +.00000000 +00000-0 +10929-2 0 00002
2 00053 47.2766 95.1184 0101172 327.3370 32.1191 12.17411474 06
| Epoch (UTC): | 11 May 2026 14:58:34 |
| Eccentricity: | 0.0101172 |
| inclination: | 47.2766° |
| perigee height: | 1523 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 95.1184° |
| argument of perigee: | 327.3370° |
| revolutions per day: | 12.17411474 |
| mean anomaly at epoch: | 32.1191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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