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 20439U 90005D 22268.48442394 .00000107 00000-0 56221-4 0 9998
2 20439 98.8557 247.3564 0009695 258.2933 216.4641 14.32934539706992
| Epoch (UTC): | 25 September 2022 11:37:34 |
| Eccentricity: | 0.0009695 |
| inclination: | 98.8557° |
| perigee height: | 775 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 247.3564° |
| argument of perigee: | 258.2933° |
| revolutions per day: | 14.32934539 |
| mean anomaly at epoch: | 216.4641° |
| orbit number at epoch: | 70699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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