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 40516U 95015DC 24355.79378376 .00008418 00000-0 32416-2 0 9994
2 40516 98.8218 11.6731 0024893 284.6628 75.1794 14.30385147504575
Epoch (UTC): | 20 December 2024 19:03:02 |
Eccentricity: | 0.0024893 |
inclination: | 98.8218° |
perigee height: | 772 km |
apogee height: | 808 km |
right ascension of ascending node: | 11.6731° |
argument of perigee: | 284.6628° |
revolutions per day: | 14.30385147 |
mean anomaly at epoch: | 75.1794° |
orbit number at epoch: | 50457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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