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 41655U 00055NU 22228.02246323 .00001543 00000-0 75061-3 0 9994
2 41655 98.7610 311.5025 0020605 258.3435 101.5428 14.19589649327395
| Epoch (UTC): | 16 August 2022 00:32:20 |
| Eccentricity: | 0.0020605 |
| inclination: | 98.7610° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 311.5025° |
| argument of perigee: | 258.3435° |
| revolutions per day: | 14.19589649 |
| mean anomaly at epoch: | 101.5428° |
| orbit number at epoch: | 32739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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