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 is defined by the following mean orbital elements,
1 43049U 17071N 22255.05173450 .15425766 12621-4 25874-3 0 9998
2 43049 51.6097 313.3868 0002955 270.4685 89.6006 16.47958215269368
| Epoch (UTC): | 12 September 2022 01:14:29 |
| Eccentricity: | 0.0002955 |
| inclination: | 51.6097° |
| perigee height: | 143 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 313.3868° |
| argument of perigee: | 270.4685° |
| revolutions per day: | 16.47958215 |
| mean anomaly at epoch: | 89.6006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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