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 12988U 81117B 22145.58193196 .00000471 00000-0 52292-4 0 9998
2 12988 82.5245 181.5246 0018250 13.8531 346.3182 14.84946327187405
Epoch (UTC): | 25 May 2022 13:57:58 |
Eccentricity: | 0.0018250 |
inclination: | 82.5245° |
perigee height: | 601 km |
apogee height: | 626 km |
right ascension of ascending node: | 181.5246° |
argument of perigee: | 13.8531° |
revolutions per day: | 14.84946327 |
mean anomaly at epoch: | 346.3182° |
orbit number at epoch: | 18740 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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