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 44879U 19093A 22176.86787914 .00001304 00000-0 16955-3 0 9999
2 44879 97.8956 256.2726 0016010 151.7092 208.4968 14.82290264136040
| Epoch (UTC): | 25 June 2022 20:49:44 |
| Eccentricity: | 0.0016010 |
| inclination: | 97.8956° |
| perigee height: | 611 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 256.2726° |
| argument of perigee: | 151.7092° |
| revolutions per day: | 14.82290264 |
| mean anomaly at epoch: | 208.4968° |
| orbit number at epoch: | 13604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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