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 23091.11886260 .00007231 00000-0 80310-3 0 9995
2 40074 98.3480 351.5815 0005348 68.6259 291.5503 14.87522197472793
| Epoch (UTC): | 01 April 2023 02:51:09 |
| Eccentricity: | 0.0005348 |
| inclination: | 98.3480° |
| perigee height: | 602 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 351.5815° |
| argument of perigee: | 68.6259° |
| revolutions per day: | 14.87522197 |
| mean anomaly at epoch: | 291.5503° |
| orbit number at epoch: | 47279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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