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 61542U 26145.60099660 +.00000000 +00000-0 +16072-4 0 00005
2 61542 53.1578 217.3739 0000993 73.1098 287.0028 15.69710187 02
| Epoch (UTC): | 25 May 2026 14:25:26 |
| Eccentricity: | 0.0000993 |
| inclination: | 53.1578° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 217.3739° |
| argument of perigee: | 73.1098° |
| revolutions per day: | 15.69710187 |
| mean anomaly at epoch: | 287.0028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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