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 55015U 23001G 25342.27629576 .00011751 00000-0 33678-3 0 9997
2 55015 97.3605 45.0386 0008862 76.6978 283.5254 15.36022558163007
| Epoch (UTC): | 08 December 2025 06:37:51 |
| Eccentricity: | 0.0008862 |
| inclination: | 97.3605° |
| perigee height: | 452 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 45.0386° |
| argument of perigee: | 76.6978° |
| revolutions per day: | 15.36022558 |
| mean anomaly at epoch: | 283.5254° |
| orbit number at epoch: | 16300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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