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 22285U 92093B 25163.13821998 -.00000228 00000-0 -92333-4 0 9998
2 22285 71.0209 212.2009 0004972 331.0731 29.0116 14.15397677675193
Epoch (UTC): | 12 June 2025 03:19:02 |
Eccentricity: | 0.0004972 |
inclination: | 71.0209° |
perigee height: | 837 km |
apogee height: | 844 km |
right ascension of ascending node: | 212.2009° |
argument of perigee: | 331.0731° |
revolutions per day: | 14.15397677 |
mean anomaly at epoch: | 29.0116° |
orbit number at epoch: | 67519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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