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 48274U 21035A 22136.08193446 .00024767 00000-0 30489-3 0 9998
2 48274 41.4711 54.0865 0003565 348.2368 142.2699 15.59648498 59754
Epoch (UTC): | 16 May 2022 01:57:59 |
Eccentricity: | 0.0003565 |
inclination: | 41.4711° |
perigee height: | 386 km |
apogee height: | 391 km |
right ascension of ascending node: | 54.0865° |
argument of perigee: | 348.2368° |
revolutions per day: | 15.59648498 |
mean anomaly at epoch: | 142.2699° |
orbit number at epoch: | 5975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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