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 data is extracted from the following two-line orbital elements,
1 07530U 74089B 23079.71334325 -.00000035 00000-0 70563-4 0 9996
2 07530 101.9420 65.8127 0011937 232.1583 301.0582 12.53662463212088
| Epoch (UTC): | 20 March 2023 17:07:12 |
| Eccentricity: | 0.0011937 |
| inclination: | 101.9420° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 65.8127° |
| argument of perigee: | 232.1583° |
| revolutions per day: | 12.53662463 |
| mean anomaly at epoch: | 301.0582° |
| orbit number at epoch: | 21208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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