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 22445U 92093EN 24358.24695733 .00001693 00000-0 88067-3 0 9992
2 22445 71.2883 42.7015 0078120 312.2972 47.1547 14.14458105642150
| Epoch (UTC): | 23 December 2024 05:55:37 |
| Eccentricity: | 0.0078120 |
| inclination: | 71.2883° |
| perigee height: | 788 km |
| apogee height: | 900 km |
| right ascension of ascending node: | 42.7015° |
| argument of perigee: | 312.2972° |
| revolutions per day: | 14.14458105 |
| mean anomaly at epoch: | 47.1547° |
| orbit number at epoch: | 64215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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