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 26041.53604394 +.00000000 +00000-0 +19516-3 0 00005
2 25544 51.6312 206.5863 0011092 84.3744 275.8509 15.48525084 01
| Epoch (UTC): | 10 February 2026 12:51:54 |
| Eccentricity: | 0.0011092 |
| inclination: | 51.6312° |
| perigee height: | 413 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 206.5863° |
| argument of perigee: | 84.3744° |
| revolutions per day: | 15.48525084 |
| mean anomaly at epoch: | 275.8509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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