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 41590U 16038C 23038.13776060 .00000104 00000-0 64590-3 0 9995
2 41590 22.1465 237.9646 8189536 190.1471 123.7915 1.18384640 28688
| Epoch (UTC): | 07 February 2023 03:18:22 |
| Eccentricity: | 0.8189536 |
| inclination: | 22.1465° |
| perigee height: | 455 km |
| apogee height: | 62279 km |
| right ascension of ascending node: | 237.9646° |
| argument of perigee: | 190.1471° |
| revolutions per day: | 1.18384640 |
| mean anomaly at epoch: | 123.7915° |
| orbit number at epoch: | 2868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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