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 23149.80932190 .00000395 00000-0 23610-3 0 9990
2 27433 99.0513 176.1667 0015434 56.9379 303.3273 14.13010165 83855
| Epoch (UTC): | 29 May 2023 19:25:25 |
| Eccentricity: | 0.0015434 |
| inclination: | 99.0513° |
| perigee height: | 838 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 176.1667° |
| argument of perigee: | 56.9379° |
| revolutions per day: | 14.13010165 |
| mean anomaly at epoch: | 303.3273° |
| orbit number at epoch: | 8385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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