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 04071U 69070B 22228.39128129 .00000301 00000-0 64386-4 0 9990
2 04071 74.0485 108.4956 0014998 319.8613 40.1445 14.63165105813616
| Epoch (UTC): | 16 August 2022 09:23:26 |
| Eccentricity: | 0.0014998 |
| inclination: | 74.0485° |
| perigee height: | 672 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 108.4956° |
| argument of perigee: | 319.8613° |
| revolutions per day: | 14.63165105 |
| mean anomaly at epoch: | 40.1445° |
| orbit number at epoch: | 81361 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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