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 40315U 14075A 25130.67622301 .00000038 00000-0 00000-0 0 9999
2 40315 63.6140 204.3097 0021181 209.7446 150.2032 2.13101511 81271
Epoch (UTC): | 10 May 2025 16:13:45 |
Eccentricity: | 0.0021181 |
inclination: | 63.6140° |
perigee height: | 19076 km |
apogee height: | 19184 km |
right ascension of ascending node: | 204.3097° |
argument of perigee: | 209.7446° |
revolutions per day: | 2.13101511 |
mean anomaly at epoch: | 150.2032° |
orbit number at epoch: | 8127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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