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 23160.84935230 .00000049 00000-0 48959-4 0 9994
2 27432 99.0229 195.3452 0050093 348.4431 184.4711 14.14215923 87333
| Epoch (UTC): | 09 June 2023 20:23:04 |
| Eccentricity: | 0.0050093 |
| inclination: | 99.0229° |
| perigee height: | 809 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 195.3452° |
| argument of perigee: | 348.4431° |
| revolutions per day: | 14.14215923 |
| mean anomaly at epoch: | 184.4711° |
| orbit number at epoch: | 8733 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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