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 22182.85386664 .00014825 00000-0 41729-3 0 9999
2 40900 97.3985 200.9096 0007660 221.9316 262.2777 15.36540629376825
| Epoch (UTC): | 01 July 2022 20:29:34 |
| Eccentricity: | 0.0007660 |
| inclination: | 97.3985° |
| perigee height: | 451 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 200.9096° |
| argument of perigee: | 221.9316° |
| revolutions per day: | 15.36540629 |
| mean anomaly at epoch: | 262.2777° |
| orbit number at epoch: | 37682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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