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 40074U 14037F 23083.65200319 .00007937 00000-0 88329-3 0 9991
2 40074 98.3496 343.7286 0005160 90.9287 269.2610 14.87406152471686
| Epoch (UTC): | 24 March 2023 15:38:53 |
| Eccentricity: | 0.0005160 |
| inclination: | 98.3496° |
| perigee height: | 602 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 343.7286° |
| argument of perigee: | 90.9287° |
| revolutions per day: | 14.87406152 |
| mean anomaly at epoch: | 269.2610° |
| orbit number at epoch: | 47168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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