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 00045U 60007A 21026.60831911 .00000011 00000-0 29702-4 0 9998
2 00045 66.6945 152.7974 0252312 154.7213 206.6489 14.33704016 97820
Epoch (UTC): | 26 January 2021 14:35:58 |
Eccentricity: | 0.0252312 |
inclination: | 66.6945° |
perigee height: | 599 km |
apogee height: | 960 km |
right ascension of ascending node: | 152.7974° |
argument of perigee: | 154.7213° |
revolutions per day: | 14.33704016 |
mean anomaly at epoch: | 206.6489° |
orbit number at epoch: | 9782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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