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 28654U 05018A 23266.14054904 .00000331 00000-0 20126-3 0 9996
2 28654 98.9026 340.0284 0015318 102.7094 257.5792 14.13011131945408
| Epoch (UTC): | 23 September 2023 03:22:23 |
| Eccentricity: | 0.0015318 |
| inclination: | 98.9026° |
| perigee height: | 838 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 340.0284° |
| argument of perigee: | 102.7094° |
| revolutions per day: | 14.13011131 |
| mean anomaly at epoch: | 257.5792° |
| orbit number at epoch: | 94540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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