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 18344.54771836 .00000636 00000-0 41639-4 0 9993
2 41915 97.4666 52.9452 0011399 44.9146 62.5583 15.11156163105744
| Epoch (UTC): | 10 December 2018 13:08:42 |
| Eccentricity: | 0.0011399 |
| inclination: | 97.4666° |
| perigee height: | 525 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 52.9452° |
| argument of perigee: | 44.9146° |
| revolutions per day: | 15.11156163 |
| mean anomaly at epoch: | 62.5583° |
| orbit number at epoch: | 10574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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