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 26160.19103139 +.00000000 +00000-0 +12924-3 0 00006
2 25544 51.6332 339.6717 0006890 149.5560 210.5830 15.49678250 07
| Epoch (UTC): | 09 June 2026 04:35:05 |
| Eccentricity: | 0.0006890 |
| inclination: | 51.6332° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 339.6717° |
| argument of perigee: | 149.5560° |
| revolutions per day: | 15.49678250 |
| mean anomaly at epoch: | 210.5830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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