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 30736U 99025ASW 23267.82111219 .00001957 00000-0 21435-2 0 9998
2 30736 98.8182 15.3921 0289143 358.9407 153.6688 13.56936536818484
| Epoch (UTC): | 24 September 2023 19:42:24 |
| Eccentricity: | 0.0289143 |
| inclination: | 98.8182° |
| perigee height: | 832 km |
| apogee height: | 1261 km |
| right ascension of ascending node: | 15.3921° |
| argument of perigee: | 358.9407° |
| revolutions per day: | 13.56936536 |
| mean anomaly at epoch: | 153.6688° |
| orbit number at epoch: | 81848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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