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 07530U 26106.80566242 +.00000000 +00000-0 +40452-4 0 00005
2 07530 101.9942 119.4056 0011891 247.5514 296.5364 12.53697138 07
| Epoch (UTC): | 16 April 2026 19:20:09 |
| Eccentricity: | 0.0011891 |
| inclination: | 101.9942° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 119.4056° |
| argument of perigee: | 247.5514° |
| revolutions per day: | 12.53697138 |
| mean anomaly at epoch: | 296.5364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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