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 31313U 99025BPR 24358.16705007 .00001182 00000-0 55465-3 0 9994
2 31313 99.0428 247.8597 0046084 116.3586 244.2333 14.21566021920582
| Epoch (UTC): | 23 December 2024 04:00:33 |
| Eccentricity: | 0.0046084 |
| inclination: | 99.0428° |
| perigee height: | 787 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 247.8597° |
| argument of perigee: | 116.3586° |
| revolutions per day: | 14.21566021 |
| mean anomaly at epoch: | 244.2333° |
| orbit number at epoch: | 92058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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