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 870U 64051A 21068.15801167 .00000053 00000-0 35959-4 0 9990
2 870 79.8984 213.4825 0097020 302.8703 56.3143 13.91172227866050
Epoch (UTC): | 09 March 2021 03:47:32 |
Eccentricity: | 0.0097020 |
inclination: | 79.8984° |
perigee height: | 853 km |
apogee height: | 995 km |
right ascension of ascending node: | 213.4825° |
argument of perigee: | 302.8703° |
revolutions per day: | 13.91172227 |
mean anomaly at epoch: | 56.3143° |
orbit number at epoch: | 86605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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