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 31624U 99025CAE 23340.20712522 .00011179 00000-0 26470-2 0 9994
2 31624 99.6501 69.5599 0043363 316.6586 74.0821 14.53679535866634
| Epoch (UTC): | 06 December 2023 04:58:15 |
| Eccentricity: | 0.0043363 |
| inclination: | 99.6501° |
| perigee height: | 683 km |
| apogee height: | 744 km |
| right ascension of ascending node: | 69.5599° |
| argument of perigee: | 316.6586° |
| revolutions per day: | 14.53679535 |
| mean anomaly at epoch: | 74.0821° |
| orbit number at epoch: | 86663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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