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 22676U 93036B 22227.39812994 .00000116 00000-0 50663-4 0 9996
2 22676 74.0445 333.6159 0019808 260.2628 99.6287 14.34129225525265
Epoch (UTC): | 15 August 2022 09:33:18 |
Eccentricity: | 0.0019808 |
inclination: | 74.0445° |
perigee height: | 764 km |
apogee height: | 792 km |
right ascension of ascending node: | 333.6159° |
argument of perigee: | 260.2628° |
revolutions per day: | 14.34129225 |
mean anomaly at epoch: | 99.6287° |
orbit number at epoch: | 52526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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