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 22229.49083239 .00000136 00000-0 57871-4 0 9991
2 22676 74.0445 329.7878 0019780 256.1671 103.7280 14.34129948525879
Epoch (UTC): | 17 August 2022 11:46:47 |
Eccentricity: | 0.0019780 |
inclination: | 74.0445° |
perigee height: | 764 km |
apogee height: | 792 km |
right ascension of ascending node: | 329.7878° |
argument of perigee: | 256.1671° |
revolutions per day: | 14.34129948 |
mean anomaly at epoch: | 103.7280° |
orbit number at epoch: | 52587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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