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 23341.19414285 .00004705 00000-0 48792-3 0 9996
2 40074 98.3387 254.9015 0004274 10.1805 349.9497 14.90508190510001
| Epoch (UTC): | 07 December 2023 04:39:33 |
| Eccentricity: | 0.0004274 |
| inclination: | 98.3387° |
| perigee height: | 593 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 254.9015° |
| argument of perigee: | 10.1805° |
| revolutions per day: | 14.90508190 |
| mean anomaly at epoch: | 349.9497° |
| orbit number at epoch: | 51000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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