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 58U 60013A 24251.16107307 .00000144 00000-0 84595-4 0 9996
2 58 28.3270 187.8294 0164909 241.8821 116.4967 13.46384128147209
Epoch (UTC): | 07 September 2024 03:51:56 |
Eccentricity: | 0.0164909 |
inclination: | 28.3270° |
perigee height: | 962 km |
apogee height: | 1208 km |
right ascension of ascending node: | 187.8294° |
argument of perigee: | 241.8821° |
revolutions per day: | 13.46384128 |
mean anomaly at epoch: | 116.4967° |
orbit number at epoch: | 14720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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