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 26041.47150897 +.00000000 +00000-0 +18993-3 0 00000
2 25544 51.6313 206.9057 0011100 84.3131 275.9122 15.48523328 02
| Epoch (UTC): | 10 February 2026 11:18:58 |
| Eccentricity: | 0.0011100 |
| inclination: | 51.6313° |
| perigee height: | 413 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 206.9057° |
| argument of perigee: | 84.3131° |
| revolutions per day: | 15.48523328 |
| mean anomaly at epoch: | 275.9122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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