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 22488U 93008B 24306.59581222 .00000294 00000-0 27766-3 0 9999
2 22488 82.9437 233.1210 0024026 232.1792 301.4561 13.77911688594987
Epoch (UTC): | 01 November 2024 14:17:58 |
Eccentricity: | 0.0024026 |
inclination: | 82.9437° |
perigee height: | 953 km |
apogee height: | 989 km |
right ascension of ascending node: | 233.1210° |
argument of perigee: | 232.1792° |
revolutions per day: | 13.77911688 |
mean anomaly at epoch: | 301.4561° |
orbit number at epoch: | 59498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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