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 26068.64624531 +.00000000 +00000-0 +13108-4 0 00008
2 07530 101.9969 80.8356 0011970 322.2073 149.4746 12.53696308 07
| Epoch (UTC): | 09 March 2026 15:30:35 |
| Eccentricity: | 0.0011970 |
| inclination: | 101.9969° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 80.8356° |
| argument of perigee: | 322.2073° |
| revolutions per day: | 12.53696308 |
| mean anomaly at epoch: | 149.4746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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