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 28057U 26053.83738747 +.00000000 +00000-0 +90386-4 0 00008
2 28057 98.7423 23.8372 0001809 105.7662 254.3723 14.36690477 00
| Epoch (UTC): | 22 February 2026 20:05:50 |
| Eccentricity: | 0.0001809 |
| inclination: | 98.7423° |
| perigee height: | 768 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 23.8372° |
| argument of perigee: | 105.7662° |
| revolutions per day: | 14.36690477 |
| mean anomaly at epoch: | 254.3723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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