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 23340.58995464 .00005590 00000-0 57855-3 0 9994
2 40074 98.3385 254.2640 0004326 11.9871 348.1448 14.90502293509919
| Epoch (UTC): | 06 December 2023 14:09:32 |
| Eccentricity: | 0.0004326 |
| inclination: | 98.3385° |
| perigee height: | 593 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 254.2640° |
| argument of perigee: | 11.9871° |
| revolutions per day: | 14.90502293 |
| mean anomaly at epoch: | 348.1448° |
| orbit number at epoch: | 50991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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