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 36095U 09063A 24279.51152906 .00000199 00000-0 19676-3 0 9995
2 36095 67.1488 319.8435 0008323 251.2955 108.7227 13.96939856758766
Epoch (UTC): | 05 October 2024 12:16:36 |
Eccentricity: | 0.0008323 |
inclination: | 67.1488° |
perigee height: | 898 km |
apogee height: | 910 km |
right ascension of ascending node: | 319.8435° |
argument of perigee: | 251.2955° |
revolutions per day: | 13.96939856 |
mean anomaly at epoch: | 108.7227° |
orbit number at epoch: | 75876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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