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 25338U 98030A 23151.74177465 .00000249 00000-0 12164-3 0 9996
2 25338 98.6064 181.0792 0010381 9.0079 351.1286 14.26324139302918
| Epoch (UTC): | 31 May 2023 17:48:09 |
| Eccentricity: | 0.0010381 |
| inclination: | 98.6064° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 181.0792° |
| argument of perigee: | 9.0079° |
| revolutions per day: | 14.26324139 |
| mean anomaly at epoch: | 351.1286° |
| orbit number at epoch: | 30291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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