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 23153.49143990 .00000486 00000-0 28495-3 0 9999
2 27433 99.0510 179.8897 0015315 47.1235 313.1220 14.13014028 84391
| Epoch (UTC): | 02 June 2023 11:47:40 |
| Eccentricity: | 0.0015315 |
| inclination: | 99.0510° |
| perigee height: | 838 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 179.8897° |
| argument of perigee: | 47.1235° |
| revolutions per day: | 14.13014028 |
| mean anomaly at epoch: | 313.1220° |
| orbit number at epoch: | 8439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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