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 26040.56801308 +.00000000 +00000-0 +17540-3 0 00006
2 25544 51.6311 211.3720 0011129 80.8535 279.3711 15.48504497 05
| Epoch (UTC): | 09 February 2026 13:37:56 |
| Eccentricity: | 0.0011129 |
| inclination: | 51.6311° |
| perigee height: | 414 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 211.3720° |
| argument of perigee: | 80.8535° |
| revolutions per day: | 15.48504497 |
| mean anomaly at epoch: | 279.3711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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