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 17304U 87006B 24281.58025628 .00001587 00000-0 52451-3 0 9990
2 17304 74.0582 222.4439 0028077 113.9784 246.4315 14.38593738976734
Epoch (UTC): | 07 October 2024 13:55:34 |
Eccentricity: | 0.0028077 |
inclination: | 74.0582° |
perigee height: | 743 km |
apogee height: | 783 km |
right ascension of ascending node: | 222.4439° |
argument of perigee: | 113.9784° |
revolutions per day: | 14.38593738 |
mean anomaly at epoch: | 246.4315° |
orbit number at epoch: | 97673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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