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 is defined by the following mean orbital elements,
1 41170U 15077E 23343.13624618 .00570238 00000-0 16153-2 0 9992
2 41170 14.9813 308.5244 0005515 185.4524 174.5748 15.90738573443322
| Epoch (UTC): | 09 December 2023 03:16:11 |
| Eccentricity: | 0.0005515 |
| inclination: | 14.9813° |
| perigee height: | 296 km |
| apogee height: | 304 km |
| right ascension of ascending node: | 308.5244° |
| argument of perigee: | 185.4524° |
| revolutions per day: | 15.90738573 |
| mean anomaly at epoch: | 174.5748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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