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 00115U 60002D 23080.76534909 .00003463 00000-0 41604-3 0 9995
2 00115 48.1636 106.3751 0033656 11.1365 349.0286 14.85748870341439
Epoch (UTC): | 21 March 2023 18:22:06 |
Eccentricity: | 0.0033656 |
inclination: | 48.1636° |
perigee height: | 588 km |
apogee height: | 635 km |
right ascension of ascending node: | 106.3751° |
argument of perigee: | 11.1365° |
revolutions per day: | 14.85748870 |
mean anomaly at epoch: | 349.0286° |
orbit number at epoch: | 34143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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