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 41789U 16059G 22268.36017910 .00000432 00000-0 89292-4 0 9990
2 41789 97.9084 310.6804 0027611 198.0714 161.9514 14.64779798320494
| Epoch (UTC): | 25 September 2022 08:38:39 |
| Eccentricity: | 0.0027611 |
| inclination: | 97.9084° |
| perigee height: | 658 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 310.6804° |
| argument of perigee: | 198.0714° |
| revolutions per day: | 14.64779798 |
| mean anomaly at epoch: | 161.9514° |
| orbit number at epoch: | 32049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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