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 27432U 02024C 23159.13058403 .00000063 00000-0 56415-4 0 9994
2 27432 99.0231 193.6092 0050173 353.3249 73.8942 14.14215659 87094
| Epoch (UTC): | 08 June 2023 03:08:02 |
| Eccentricity: | 0.0050173 |
| inclination: | 99.0231° |
| perigee height: | 809 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 193.6092° |
| argument of perigee: | 353.3249° |
| revolutions per day: | 14.14215659 |
| mean anomaly at epoch: | 73.8942° |
| orbit number at epoch: | 8709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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