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 40030U 26118.42724867 +.00000000 +00000-0 +39112-3 0 00007
2 40030 98.0862 113.0243 0009360 54.0331 306.1766 15.14345142 09
| Epoch (UTC): | 28 April 2026 10:15:14 |
| Eccentricity: | 0.0009360 |
| inclination: | 98.0862° |
| perigee height: | 517 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 113.0243° |
| argument of perigee: | 54.0331° |
| revolutions per day: | 15.14345142 |
| mean anomaly at epoch: | 306.1766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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