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 31630U 99025CAL 23323.65101803 .00005921 00000-0 54508-3 0 9997
2 31630 98.0281 106.6754 0270887 306.4596 51.1918 14.71187778873786
| Epoch (UTC): | 19 November 2023 15:37:27 |
| Eccentricity: | 0.0270887 |
| inclination: | 98.0281° |
| perigee height: | 467 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 106.6754° |
| argument of perigee: | 306.4596° |
| revolutions per day: | 14.71187778 |
| mean anomaly at epoch: | 51.1918° |
| orbit number at epoch: | 87378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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