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 20438U 90005C 22268.53478104 .00000053 00000-0 37703-4 0 9995
2 20438 98.9293 274.9161 0009995 12.1728 100.4403 14.31144880705796
| Epoch (UTC): | 25 September 2022 12:50:05 |
| Eccentricity: | 0.0009995 |
| inclination: | 98.9293° |
| perigee height: | 781 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 274.9161° |
| argument of perigee: | 12.1728° |
| revolutions per day: | 14.31144880 |
| mean anomaly at epoch: | 100.4403° |
| orbit number at epoch: | 70579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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