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 44530U 26112.29095838 +.00000000 +00000-0 +88204-3 0 00000
2 44530 98.6374 273.6924 0009859 126.1130 234.0989 14.71458015 04
| Epoch (UTC): | 22 April 2026 06:58:58 |
| Eccentricity: | 0.0009859 |
| inclination: | 98.6374° |
| perigee height: | 649 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 273.6924° |
| argument of perigee: | 126.1130° |
| revolutions per day: | 14.71458015 |
| mean anomaly at epoch: | 234.0989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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