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 36074U 93036AYM 25138.89500035 .00004245 00000-0 12802-2 0 9990
2 36074 73.9947 7.3089 0047923 149.1039 211.2953 14.42130100829121
Epoch (UTC): | 18 May 2025 21:28:48 |
Eccentricity: | 0.0047923 |
inclination: | 73.9947° |
perigee height: | 717 km |
apogee height: | 785 km |
right ascension of ascending node: | 7.3089° |
argument of perigee: | 149.1039° |
revolutions per day: | 14.42130100 |
mean anomaly at epoch: | 211.2953° |
orbit number at epoch: | 82912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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