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 18985U 88023A 24358.07631279 .00000096 00000-0 82357-4 0 9993
2 18985 82.9555 196.2340 0040676 200.9431 159.0062 13.76616339721811
| Epoch (UTC): | 23 December 2024 01:49:53 |
| Eccentricity: | 0.0040676 |
| inclination: | 82.9555° |
| perigee height: | 946 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 196.2340° |
| argument of perigee: | 200.9431° |
| revolutions per day: | 13.76616339 |
| mean anomaly at epoch: | 159.0062° |
| orbit number at epoch: | 72181 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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