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 26140.48941956 +.00000000 +00000-0 -13141-5 0 00006
2 00053 47.2782 67.7707 0100972 353.6472 6.3033 12.17412659 06
| Epoch (UTC): | 20 May 2026 11:44:45 |
| Eccentricity: | 0.0100972 |
| inclination: | 47.2782° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 67.7707° |
| argument of perigee: | 353.6472° |
| revolutions per day: | 12.17412659 |
| mean anomaly at epoch: | 6.3033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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