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 27433U 02024D 23151.57957220 .00000444 00000-0 26223-3 0 9996
2 27433 99.0512 177.9567 0015362 52.2139 308.0421 14.13012024 84107
| Epoch (UTC): | 31 May 2023 13:54:35 |
| Eccentricity: | 0.0015362 |
| inclination: | 99.0512° |
| perigee height: | 838 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 177.9567° |
| argument of perigee: | 52.2139° |
| revolutions per day: | 14.13012024 |
| mean anomaly at epoch: | 308.0421° |
| orbit number at epoch: | 8410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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