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 15453U 84129A 23273.84503439 -.00000153 00000-0 00000+0 0 9994
2 15453 13.1062 328.5414 0004594 195.1501 161.4487 0.98857593 16242
| Epoch (UTC): | 30 September 2023 20:16:50 |
| Eccentricity: | 0.0004594 |
| inclination: | 13.1062° |
| perigee height: | 36168 km |
| apogee height: | 36207 km |
| right ascension of ascending node: | 328.5414° |
| argument of perigee: | 195.1501° |
| revolutions per day: | 0.98857593 |
| mean anomaly at epoch: | 161.4487° |
| orbit number at epoch: | 1624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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