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 23605U 95033A 25189.90216130 0.00002200 00000-0 16223-3 0 07
2 23605 98.2499 53.5267 0015406 137.2307 222.7691 15.03259318 02
| Epoch (UTC): | 08 July 2025 21:39:06 |
| Eccentricity: | 0.0015406 |
| inclination: | 98.2499° |
| perigee height: | 546 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 53.5267° |
| argument of perigee: | 137.2307° |
| revolutions per day: | 15.03259318 |
| mean anomaly at epoch: | 222.7691° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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