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 26133.18366502 +.00000000 +00000-0 +13039-2 0 00005
2 00053 47.2768 90.3072 0101135 331.9630 27.5736 12.17412016 06
| Epoch (UTC): | 13 May 2026 04:24:28 |
| Eccentricity: | 0.0101135 |
| inclination: | 47.2768° |
| perigee height: | 1523 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 90.3072° |
| argument of perigee: | 331.9630° |
| revolutions per day: | 12.17412016 |
| mean anomaly at epoch: | 27.5736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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