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 34810U 09020A 22263.24097000 0.00000000 00000-0 00000-0 0 07
2 34810 0.1150 97.5522 0003453 144.1930 215.8462 1.00270000 00
| Epoch (UTC): | 20 September 2022 05:46:59 |
| Eccentricity: | 0.0003453 |
| inclination: | 0.1150° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 97.5522° |
| argument of perigee: | 144.1930° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 215.8462° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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