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 8027U 75064B 23152.19099780 .00000011 00000-0 -84074-6 0 9997
2 8027 81.2970 120.6555 0049309 247.8430 111.7502 14.07470744458409
| Epoch (UTC): | 01 June 2023 04:35:02 |
| Eccentricity: | 0.0049309 |
| inclination: | 81.2970° |
| perigee height: | 832 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 120.6555° |
| argument of perigee: | 247.8430° |
| revolutions per day: | 14.07470744 |
| mean anomaly at epoch: | 111.7502° |
| orbit number at epoch: | 45840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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