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 40028U 26053.77219515 +.00000000 +00000-0 +44607-3 0 00004
2 40028 98.1020 57.2941 0005629 210.7678 149.3223 15.13479728 08
| Epoch (UTC): | 22 February 2026 18:31:57 |
| Eccentricity: | 0.0005629 |
| inclination: | 98.1020° |
| perigee height: | 522 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 57.2941° |
| argument of perigee: | 210.7678° |
| revolutions per day: | 15.13479728 |
| mean anomaly at epoch: | 149.3223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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