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 22136.56599520 .00005871 00000-0 60657-3 0 9995
2 39770 97.9366 253.3236 0008768 184.7090 175.4213 14.90495104432919
Epoch (UTC): | 16 May 2022 13:35:01 |
Eccentricity: | 0.0008768 |
inclination: | 97.9366° |
perigee height: | 590 km |
apogee height: | 602 km |
right ascension of ascending node: | 253.3236° |
argument of perigee: | 184.7090° |
revolutions per day: | 14.90495104 |
mean anomaly at epoch: | 175.4213° |
orbit number at epoch: | 43291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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