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 31118U 07012B 23274.41903220 .00000788 00000-0 14002-3 0 9996
2 31118 98.0218 216.7791 0015954 132.9569 227.2978 14.69812167882321
| Epoch (UTC): | 01 October 2023 10:03:24 |
| Eccentricity: | 0.0015954 |
| inclination: | 98.0218° |
| perigee height: | 650 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 216.7791° |
| argument of perigee: | 132.9569° |
| revolutions per day: | 14.69812167 |
| mean anomaly at epoch: | 227.2978° |
| orbit number at epoch: | 88232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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