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 24259.36710311 .00018009 00000-0 15957-2 0 9991
2 40074 98.3430 194.9749 0006551 119.1238 241.0638 14.96284499552258
| Epoch (UTC): | 15 September 2024 08:48:37 |
| Eccentricity: | 0.0006551 |
| inclination: | 98.3430° |
| perigee height: | 574 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 194.9749° |
| argument of perigee: | 119.1238° |
| revolutions per day: | 14.96284499 |
| mean anomaly at epoch: | 241.0638° |
| orbit number at epoch: | 55225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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