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 40021U 14033M 23081.67636399 .00011708 00000-0 10379-2 0 9990
2 40021 98.0494 43.0002 0010639 192.2661 167.8302 14.96340310476249
| Epoch (UTC): | 22 March 2023 16:13:57 |
| Eccentricity: | 0.0010639 |
| inclination: | 98.0494° |
| perigee height: | 571 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 43.0002° |
| argument of perigee: | 192.2661° |
| revolutions per day: | 14.96340310 |
| mean anomaly at epoch: | 167.8302° |
| orbit number at epoch: | 47624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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