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 27513U 26145.38257727 +.00000000 +00000-0 +00000-0 0 00000
2 27513 5.7460 73.1970 0004633 347.4952 24.1496 1.00271558 04
| Epoch (UTC): | 25 May 2026 09:10:54 |
| Eccentricity: | 0.0004633 |
| inclination: | 5.7460° |
| perigee height: | 35767 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 73.1970° |
| argument of perigee: | 347.4952° |
| revolutions per day: | 1.00271558 |
| mean anomaly at epoch: | 24.1496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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