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 22888U 93070A 24286.46208139 .00000191 00000-0 18169-3 0 9991
2 22888 82.9538 174.6959 0049538 96.9405 75.3420 13.75089235549819
| Epoch (UTC): | 12 October 2024 11:05:23 |
| Eccentricity: | 0.0049538 |
| inclination: | 82.9538° |
| perigee height: | 945 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 174.6959° |
| argument of perigee: | 96.9405° |
| revolutions per day: | 13.75089235 |
| mean anomaly at epoch: | 75.3420° |
| orbit number at epoch: | 54981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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