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 00085U 61004C 21023.26955544 .00001954 00000-0 41524-3 0 9990
2 00085 38.7769 338.9074 0394507 165.6805 195.5501 14.21569340962376
Epoch (UTC): | 23 January 2021 06:28:09 |
Eccentricity: | 0.0394507 |
inclination: | 38.7769° |
perigee height: | 536 km |
apogee height: | 1104 km |
right ascension of ascending node: | 338.9074° |
argument of perigee: | 165.6805° |
revolutions per day: | 14.21569340 |
mean anomaly at epoch: | 195.5501° |
orbit number at epoch: | 96237 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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