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 40379U 15003D 23088.73121696 .00038450 00000-0 99220-3 0 9993
2 40379 99.0785 6.7817 0091947 182.7200 177.3551 15.34767719451179
| Epoch (UTC): | 29 March 2023 17:32:57 |
| Eccentricity: | 0.0091947 |
| inclination: | 99.0785° |
| perigee height: | 399 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 6.7817° |
| argument of perigee: | 182.7200° |
| revolutions per day: | 15.34767719 |
| mean anomaly at epoch: | 177.3551° |
| orbit number at epoch: | 45117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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