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 35752U 26145.34250110 +.00000000 +00000-0 +00000-0 0 00009
2 35752 56.1964 28.3489 0053523 82.2755 30.1700 2.00555521 02
| Epoch (UTC): | 25 May 2026 08:13:12 |
| Eccentricity: | 0.0053523 |
| inclination: | 56.1964° |
| perigee height: | 20041 km |
| apogee height: | 20325 km |
| right ascension of ascending node: | 28.3489° |
| argument of perigee: | 82.2755° |
| revolutions per day: | 2.00555521 |
| mean anomaly at epoch: | 30.1700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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