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 23083.58573917 .00001139 00000-0 19952-3 0 9998
2 31118 98.0052 29.4224 0015787 28.9409 331.2669 14.69589575854290
| Epoch (UTC): | 24 March 2023 14:03:27 |
| Eccentricity: | 0.0015787 |
| inclination: | 98.0052° |
| perigee height: | 651 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 29.4224° |
| argument of perigee: | 28.9409° |
| revolutions per day: | 14.69589575 |
| mean anomaly at epoch: | 331.2669° |
| orbit number at epoch: | 85429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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