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 35869U 09049E 25194.14440286 .00000040 00000-0 37068-4 0 9995
2 35869 98.6879 154.3619 0004036 189.7477 170.3624 14.23098127821286
Epoch (UTC): | 13 July 2025 03:27:56 |
Eccentricity: | 0.0004036 |
inclination: | 98.6879° |
perigee height: | 812 km |
apogee height: | 818 km |
right ascension of ascending node: | 154.3619° |
argument of perigee: | 189.7477° |
revolutions per day: | 14.23098127 |
mean anomaly at epoch: | 170.3624° |
orbit number at epoch: | 82128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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