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 41915U 17002C 19047.88414255 .00000559 00000-0 36970-4 0 9996
2 41915 97.4573 119.6233 0010780 154.7939 326.3097 15.11219198116068
| Epoch (UTC): | 16 February 2019 21:13:09 |
| Eccentricity: | 0.0010780 |
| inclination: | 97.4573° |
| perigee height: | 525 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 119.6233° |
| argument of perigee: | 154.7939° |
| revolutions per day: | 15.11219198 |
| mean anomaly at epoch: | 326.3097° |
| orbit number at epoch: | 11606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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