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 35935U 09051E 23271.63117068 .00001473 00000-0 33886-3 0 9993
2 35935 98.5067 145.5026 0009217 68.2510 291.9668 14.56904225744055
Epoch (UTC): | 28 September 2023 15:08:53 |
Eccentricity: | 0.0009217 |
inclination: | 98.5067° |
perigee height: | 696 km |
apogee height: | 710 km |
right ascension of ascending node: | 145.5026° |
argument of perigee: | 68.2510° |
revolutions per day: | 14.56904225 |
mean anomaly at epoch: | 291.9668° |
orbit number at epoch: | 74405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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