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 40910U 15049M 23087.12451584 .00042378 00000-0 13337-2 0 9996
2 40910 97.4676 99.2064 0012625 64.7528 8.7767 15.32741082416451
Epoch (UTC): | 28 March 2023 02:59:18 |
Eccentricity: | 0.0012625 |
inclination: | 97.4676° |
perigee height: | 459 km |
apogee height: | 476 km |
right ascension of ascending node: | 99.2064° |
argument of perigee: | 64.7528° |
revolutions per day: | 15.32741082 |
mean anomaly at epoch: | 8.7767° |
orbit number at epoch: | 41645 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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