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 23159.51092492 .00003809 00000-0 41912-3 0 9992
2 40074 98.3456 63.5433 0003196 194.1534 165.9592 14.88237081482960
| Epoch (UTC): | 08 June 2023 12:15:43 |
| Eccentricity: | 0.0003196 |
| inclination: | 98.3456° |
| perigee height: | 601 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 63.5433° |
| argument of perigee: | 194.1534° |
| revolutions per day: | 14.88237081 |
| mean anomaly at epoch: | 165.9592° |
| orbit number at epoch: | 48296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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