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 40908U 15049K 22176.07882787 .00002867 00000-0 15308-3 0 9998
2 40908 97.5158 176.5858 0015261 357.6000 74.1292 15.15841600373643
Epoch (UTC): | 25 June 2022 01:53:30 |
Eccentricity: | 0.0015261 |
inclination: | 97.5158° |
perigee height: | 508 km |
apogee height: | 529 km |
right ascension of ascending node: | 176.5858° |
argument of perigee: | 357.6000° |
revolutions per day: | 15.15841600 |
mean anomaly at epoch: | 74.1292° |
orbit number at epoch: | 37364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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