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 41604U 16040F 22176.53373442 .00002998 00000-0 12488-3 0 9999
2 41604 97.2102 220.6355 0013522 103.4874 256.7872 15.24388956333693
| Epoch (UTC): | 25 June 2022 12:48:34 |
| Eccentricity: | 0.0013522 |
| inclination: | 97.2102° |
| perigee height: | 483 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 220.6355° |
| argument of perigee: | 103.4874° |
| revolutions per day: | 15.24388956 |
| mean anomaly at epoch: | 256.7872° |
| orbit number at epoch: | 33369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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