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 26072.94475469 +.00000000 +00000-0 +16708-3 0 00008
2 07530 101.9966 85.1804 0011946 313.8747 110.0971 12.53696440 08
| Epoch (UTC): | 13 March 2026 22:40:26 |
| Eccentricity: | 0.0011946 |
| inclination: | 101.9966° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 85.1804° |
| argument of perigee: | 313.8747° |
| revolutions per day: | 12.53696440 |
| mean anomaly at epoch: | 110.0971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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