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 26106.97621426 +.00000000 +00000-0 +25565-3 0 00005
2 40028 98.1008 113.8845 0008133 52.6251 307.5719 15.14430557 05
| Epoch (UTC): | 16 April 2026 23:25:44 |
| Eccentricity: | 0.0008133 |
| inclination: | 98.1008° |
| perigee height: | 517 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 113.8845° |
| argument of perigee: | 52.6251° |
| revolutions per day: | 15.14430557 |
| mean anomaly at epoch: | 307.5719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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