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 26069.03498317 +.00000000 +00000-0 +20458-4 0 00009
2 07530 101.9969 81.2286 0011966 321.4313 104.0021 12.53696309 01
| Epoch (UTC): | 10 March 2026 00:50:22 |
| Eccentricity: | 0.0011966 |
| inclination: | 101.9969° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 81.2286° |
| argument of perigee: | 321.4313° |
| revolutions per day: | 12.53696309 |
| mean anomaly at epoch: | 104.0021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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