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 53497C 22099AJ 24358.51368056 .00018326 00000+0 14298-2 0 3580
2 53497 97.6546 116.6364 0004053 236.3940 167.2013 15.01231182 18
| Epoch (UTC): | 23 December 2024 12:19:42 |
| Eccentricity: | 0.0004053 |
| inclination: | 97.6546° |
| perigee height: | 560 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 116.6364° |
| argument of perigee: | 236.3940° |
| revolutions per day: | 15.01231182 |
| mean anomaly at epoch: | 167.2013° |
| 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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