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 31888U 99025CKP 23333.46943424 .00006680 00000-0 30262-2 0 9998
2 31888 99.1767 212.9980 0024540 189.5526 170.5186 14.22117725852253
| Epoch (UTC): | 29 November 2023 11:15:59 |
| Eccentricity: | 0.0024540 |
| inclination: | 99.1767° |
| perigee height: | 800 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 212.9980° |
| argument of perigee: | 189.5526° |
| revolutions per day: | 14.22117725 |
| mean anomaly at epoch: | 170.5186° |
| orbit number at epoch: | 85225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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