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 is defined by the following mean orbital elements,
1 40900U 15049B 23088.02519964 .12158542 25015-5 19349-2 0 9993
2 40900 97.3398 118.0728 0008674 252.6137 167.9130 16.33727072418695
| Epoch (UTC): | 29 March 2023 00:36:17 |
| Eccentricity: | 0.0008674 |
| inclination: | 97.3398° |
| perigee height: | 177 km |
| apogee height: | 188 km |
| right ascension of ascending node: | 118.0728° |
| argument of perigee: | 252.6137° |
| revolutions per day: | 16.33727072 |
| mean anomaly at epoch: | 167.9130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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