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 41557U 16033B 22176.13829436 .00011341 00000-0 33705-3 0 9990
2 41557 97.3880 273.8474 0010132 358.7502 85.6281 15.34877978338565
| Epoch (UTC): | 25 June 2022 03:19:08 |
| Eccentricity: | 0.0010132 |
| inclination: | 97.3880° |
| perigee height: | 454 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 273.8474° |
| argument of perigee: | 358.7502° |
| revolutions per day: | 15.34877978 |
| mean anomaly at epoch: | 85.6281° |
| orbit number at epoch: | 33856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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