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 00877U 64053B 21060.41482157 -.00000070 00000-0 11016-4 0 9992
2 00877 65.0777 298.0361 0081671 293.4099 65.8427 14.59419861998998
Epoch (UTC): | 01 March 2021 09:57:20 |
Eccentricity: | 0.0081671 |
inclination: | 65.0777° |
perigee height: | 637 km |
apogee height: | 753 km |
right ascension of ascending node: | 298.0361° |
argument of perigee: | 293.4099° |
revolutions per day: | 14.59419861 |
mean anomaly at epoch: | 65.8427° |
orbit number at epoch: | 99899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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