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 28537U 05004A 24289.79288462 0.00000700 00000-0 60745-3 0 00
2 28537 63.4004 188.5083 0497286 2.2726 357.7274 13.41057518 02
Epoch (UTC): | 15 October 2024 19:01:45 |
Eccentricity: | 0.0497286 |
inclination: | 63.4004° |
perigee height: | 733 km |
apogee height: | 1477 km |
right ascension of ascending node: | 188.5083° |
argument of perigee: | 2.2726° |
revolutions per day: | 13.41057518 |
mean anomaly at epoch: | 357.7274° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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