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 21025.51741600 .00001760 00000-0 37509-3 0 9999
2 00085 38.7776 327.4238 0394641 180.6582 179.3681 14.21576884962692
Epoch (UTC): | 25 January 2021 12:25:04 |
Eccentricity: | 0.0394641 |
inclination: | 38.7776° |
perigee height: | 536 km |
apogee height: | 1104 km |
right ascension of ascending node: | 327.4238° |
argument of perigee: | 180.6582° |
revolutions per day: | 14.21576884 |
mean anomaly at epoch: | 179.3681° |
orbit number at epoch: | 96269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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