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 35976U 93036AVS 24272.58183380 .00013318 00000-0 37071-2 0 9990
2 35976 74.0409 19.9510 0049835 200.2268 159.6918 14.45673838802446
Epoch (UTC): | 28 September 2024 13:57:50 |
Eccentricity: | 0.0049835 |
inclination: | 74.0409° |
perigee height: | 704 km |
apogee height: | 775 km |
right ascension of ascending node: | 19.9510° |
argument of perigee: | 200.2268° |
revolutions per day: | 14.45673838 |
mean anomaly at epoch: | 159.6918° |
orbit number at epoch: | 80244 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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