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 23608U 95033D 25189.52943964 .00013465 00000-0 44619-3 0 9992
2 23608 98.2900 357.1763 0010791 167.5385 192.6122 15.31381912629255
| Epoch (UTC): | 08 July 2025 12:42:23 |
| Eccentricity: | 0.0010791 |
| inclination: | 98.2900° |
| perigee height: | 464 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 357.1763° |
| argument of perigee: | 167.5385° |
| revolutions per day: | 15.31381912 |
| mean anomaly at epoch: | 192.6122° |
| orbit number at epoch: | 62925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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