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 23657U 95046A 23277.53065271 .00003749 00000-0 39970-3 0 9991
2 23657 82.5238 257.8700 0021676 25.4368 334.7911 14.88469280519195
Epoch (UTC): | 04 October 2023 12:44:08 |
Eccentricity: | 0.0021676 |
inclination: | 82.5238° |
perigee height: | 587 km |
apogee height: | 618 km |
right ascension of ascending node: | 257.8700° |
argument of perigee: | 25.4368° |
revolutions per day: | 14.88469280 |
mean anomaly at epoch: | 334.7911° |
orbit number at epoch: | 51919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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