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 39770U 14029E 22136.23033008 .00005618 00000-0 58079-3 0 9997
2 39770 97.9361 252.9850 0008881 185.7622 174.3530 14.90488633432862
Epoch (UTC): | 16 May 2022 05:31:40 |
Eccentricity: | 0.0008881 |
inclination: | 97.9361° |
perigee height: | 590 km |
apogee height: | 602 km |
right ascension of ascending node: | 252.9850° |
argument of perigee: | 185.7622° |
revolutions per day: | 14.90488633 |
mean anomaly at epoch: | 174.3530° |
orbit number at epoch: | 43286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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