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 00115U 60002D 24310.46557297 .00014778 00000-0 14461-2 0 9995
2 00115 48.1632 105.6066 0028360 136.7132 223.6019 14.92096843430016
Epoch (UTC): | 05 November 2024 11:10:25 |
Eccentricity: | 0.0028360 |
inclination: | 48.1632° |
perigee height: | 571 km |
apogee height: | 611 km |
right ascension of ascending node: | 105.6066° |
argument of perigee: | 136.7132° |
revolutions per day: | 14.92096843 |
mean anomaly at epoch: | 223.6019° |
orbit number at epoch: | 43001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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