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 26021.27150985 +.00000000 +00000-0 +37939-3 0 00005
2 25544 51.6330 306.7706 0007779 41.9176 318.2407 15.49511068 02
| Epoch (UTC): | 21 January 2026 06:30:58 |
| Eccentricity: | 0.0007779 |
| inclination: | 51.6330° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 306.7706° |
| argument of perigee: | 41.9176° |
| revolutions per day: | 15.49511068 |
| mean anomaly at epoch: | 318.2407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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