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 53468C 22099D 24358.51090278 .00021750 00000+0 16970-2 0 3580
2 53468 97.6552 116.6442 0000536 98.9720 38.2934 15.01231974 18
| Epoch (UTC): | 23 December 2024 12:15:42 |
| Eccentricity: | 0.0000536 |
| inclination: | 97.6552° |
| perigee height: | 563 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 116.6442° |
| argument of perigee: | 98.9720° |
| revolutions per day: | 15.01231974 |
| mean anomaly at epoch: | 38.2934° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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