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 40900U 15049B 22176.13660441 .00024570 00000-0 69412-3 0 9998
2 40900 97.4000 194.1543 0006913 250.6439 183.3461 15.36325215375790
| Epoch (UTC): | 25 June 2022 03:16:42 |
| Eccentricity: | 0.0006913 |
| inclination: | 97.4000° |
| perigee height: | 452 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 194.1543° |
| argument of perigee: | 250.6439° |
| revolutions per day: | 15.36325215 |
| mean anomaly at epoch: | 183.3461° |
| orbit number at epoch: | 37579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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