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 26022.53192463 +.00000000 +00000-0 +19668-4 0 00007
2 07530 101.9968 34.2284 0012356 50.1017 101.5694 12.53695239 06
| Epoch (UTC): | 22 January 2026 12:45:58 |
| Eccentricity: | 0.0012356 |
| inclination: | 101.9968° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 34.2284° |
| argument of perigee: | 50.1017° |
| revolutions per day: | 12.53695239 |
| mean anomaly at epoch: | 101.5694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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