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 03214U 68012D 25340.16406421 .00000221 00000-0 41296-3 0 9995
2 03214 89.8245 106.9287 0187155 76.2514 359.4522 13.29227116558892
| Epoch (UTC): | 06 December 2025 03:56:15 |
| Eccentricity: | 0.0187155 |
| inclination: | 89.8245° |
| perigee height: | 1009 km |
| apogee height: | 1290 km |
| right ascension of ascending node: | 106.9287° |
| argument of perigee: | 76.2514° |
| revolutions per day: | 13.29227116 |
| mean anomaly at epoch: | 359.4522° |
| orbit number at epoch: | 55889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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