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 23334.74929158 .00010230 00000-0 10552-2 0 9991
2 40074 98.3381 248.1004 0004755 25.2775 334.8673 14.90406962509040
| Epoch (UTC): | 30 November 2023 17:58:58 |
| Eccentricity: | 0.0004755 |
| inclination: | 98.3381° |
| perigee height: | 593 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 248.1004° |
| argument of perigee: | 25.2775° |
| revolutions per day: | 14.90406962 |
| mean anomaly at epoch: | 334.8673° |
| orbit number at epoch: | 50904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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