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 44071U 19014A 22269.18038990 .00000049 00000-0 00000+0 0 9992
2 44071 0.0243 174.5018 0000047 292.0021 23.7234 1.00270130 12974
| Epoch (UTC): | 26 September 2022 04:19:45 |
| Eccentricity: | 0.0000047 |
| inclination: | 0.0243° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 174.5018° |
| argument of perigee: | 292.0021° |
| revolutions per day: | 1.00270130 |
| mean anomaly at epoch: | 23.7234° |
| orbit number at epoch: | 1297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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