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 23335.75633359 .00010602 00000-0 10927-2 0 9997
2 40074 98.3380 249.1630 0004763 22.4340 337.7084 14.90426690509195
| Epoch (UTC): | 01 December 2023 18:09:07 |
| Eccentricity: | 0.0004763 |
| inclination: | 98.3380° |
| perigee height: | 593 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 249.1630° |
| argument of perigee: | 22.4340° |
| revolutions per day: | 14.90426690 |
| mean anomaly at epoch: | 337.7084° |
| orbit number at epoch: | 50919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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