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 25544U 26161.41633914 +.00000000 +00000-0 +10452-3 0 00005
2 25544 51.6361 333.6061 0005881 172.3680 187.7399 15.49162374 01
| Epoch (UTC): | 10 June 2026 09:59:31 |
| Eccentricity: | 0.0005881 |
| inclination: | 51.6361° |
| perigee height: | 415 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 333.6061° |
| argument of perigee: | 172.3680° |
| revolutions per day: | 15.49162374 |
| mean anomaly at epoch: | 187.7399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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