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 25860U 99039A 25189.39397710 .00000501 00000-0 73495-4 0 9993
2 25860 97.9824 246.2607 0001870 80.3585 279.7838 14.79832697398251
Epoch (UTC): | 08 July 2025 09:27:19 |
Eccentricity: | 0.0001870 |
inclination: | 97.9824° |
perigee height: | 628 km |
apogee height: | 631 km |
right ascension of ascending node: | 246.2607° |
argument of perigee: | 80.3585° |
revolutions per day: | 14.79832697 |
mean anomaly at epoch: | 279.7838° |
orbit number at epoch: | 39825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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