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 11963U 80073B 25082.91067130 .00000210 00000-0 10909-3 0 9997
2 11963 81.2743 254.4105 0074371 327.4190 32.2401 14.10081751289959
| Epoch (UTC): | 23 March 2025 21:51:22 |
| Eccentricity: | 0.0074371 |
| inclination: | 81.2743° |
| perigee height: | 805 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 254.4105° |
| argument of perigee: | 327.4190° |
| revolutions per day: | 14.10081751 |
| mean anomaly at epoch: | 32.2401° |
| orbit number at epoch: | 28995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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