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 26088.02669516 +.00000000 +00000-0 +15216-3 0 00005
2 07530 101.9957 100.4250 0011864 284.4165 140.2194 12.53696745 00
| Epoch (UTC): | 29 March 2026 00:38:26 |
| Eccentricity: | 0.0011864 |
| inclination: | 101.9957° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 100.4250° |
| argument of perigee: | 284.4165° |
| revolutions per day: | 12.53696745 |
| mean anomaly at epoch: | 140.2194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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