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 39497U 13076E 21016.08705884 .00000033 00000-0 16446-3 0 9999
2 39497 82.4892 322.0667 0014186 85.1592 275.1096 12.43450662320168
Epoch (UTC): | 16 January 2021 02:05:21 |
Eccentricity: | 0.0014186 |
inclination: | 82.4892° |
perigee height: | 1481 km |
apogee height: | 1503 km |
right ascension of ascending node: | 322.0667° |
argument of perigee: | 85.1592° |
revolutions per day: | 12.43450662 |
mean anomaly at epoch: | 275.1096° |
orbit number at epoch: | 32016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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