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 00059U 60013B 21015.52399788 .00000098 00000-0 90851-5 0 9999
2 00059 28.2473 208.8438 0189297 266.1429 91.7455 13.52982327975285
Epoch (UTC): | 15 January 2021 12:34:33 |
Eccentricity: | 0.0189297 |
inclination: | 28.2473° |
perigee height: | 920 km |
apogee height: | 1202 km |
right ascension of ascending node: | 208.8438° |
argument of perigee: | 266.1429° |
revolutions per day: | 13.52982327 |
mean anomaly at epoch: | 91.7455° |
orbit number at epoch: | 97528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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