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 41501U 00055LZ 22228.73110648 .00004359 00000-0 16024-2 0 9993
2 41501 98.6897 324.1049 0057314 149.3788 211.0761 14.32266231335989
| Epoch (UTC): | 16 August 2022 17:32:47 |
| Eccentricity: | 0.0057314 |
| inclination: | 98.6897° |
| perigee height: | 743 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 324.1049° |
| argument of perigee: | 149.3788° |
| revolutions per day: | 14.32266231 |
| mean anomaly at epoch: | 211.0761° |
| orbit number at epoch: | 33598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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