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 40042U 14033AJ 22027.78907158 .00001120 00000-0 12285-3 0 9994
2 40042 97.9603 325.2982 0015123 147.0226 213.1938 14.89680105413211
| Epoch (UTC): | 27 January 2022 18:56:15 |
| Eccentricity: | 0.0015123 |
| inclination: | 97.9603° |
| perigee height: | 588 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 325.2982° |
| argument of perigee: | 147.0226° |
| revolutions per day: | 14.89680105 |
| mean anomaly at epoch: | 213.1938° |
| orbit number at epoch: | 41321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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