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 27431U 02024B 23154.71641352 .00000127 00000-0 97962-4 0 9996
2 27431 99.0988 184.8851 0016481 115.5460 244.7415 14.09860921 83209
| Epoch (UTC): | 03 June 2023 17:11:38 |
| Eccentricity: | 0.0016481 |
| inclination: | 99.0988° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 184.8851° |
| argument of perigee: | 115.5460° |
| revolutions per day: | 14.09860921 |
| mean anomaly at epoch: | 244.7415° |
| orbit number at epoch: | 8320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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