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 23335.63501892 .00002252 00000-0 51003-3 0 9993
2 35935 98.4973 210.8141 0006951 223.9305 136.1340 14.57127628753342
Epoch (UTC): | 01 December 2023 15:14:25 |
Eccentricity: | 0.0006951 |
inclination: | 98.4973° |
perigee height: | 697 km |
apogee height: | 707 km |
right ascension of ascending node: | 210.8141° |
argument of perigee: | 223.9305° |
revolutions per day: | 14.57127628 |
mean anomaly at epoch: | 136.1340° |
orbit number at epoch: | 75334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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