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 26133.98839294 +.00000000 +00000-0 +11198-3 0 00008
2 07530 101.9916 146.8769 0012162 194.6235 221.6905 12.53697521 03
| Epoch (UTC): | 13 May 2026 23:43:17 |
| Eccentricity: | 0.0012162 |
| inclination: | 101.9916° |
| perigee height: | 1440 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 146.8769° |
| argument of perigee: | 194.6235° |
| revolutions per day: | 12.53697521 |
| mean anomaly at epoch: | 221.6905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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