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 12298U 81013B 24280.89192808 .00000205 00000-0 19295-3 0 9992
2 12298 82.9495 148.0696 0029566 346.1377 24.2172 13.76833281192174
Epoch (UTC): | 06 October 2024 21:24:22 |
Eccentricity: | 0.0029566 |
inclination: | 82.9495° |
perigee height: | 953 km |
apogee height: | 997 km |
right ascension of ascending node: | 148.0696° |
argument of perigee: | 346.1377° |
revolutions per day: | 13.76833281 |
mean anomaly at epoch: | 24.2172° |
orbit number at epoch: | 19217 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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