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 116U 61015A 19107.61576991 -.00000039 +00000-0 +28984-4 0 9991
2 116 066.8093 171.6548 0081560 305.2124 054.1338 13.91751016932429
| Epoch (UTC): | 17 April 2019 14:46:42 |
| Eccentricity: | 0.0081560 |
| inclination: | 66.8093° |
| perigee height: | 863 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 171.6548° |
| argument of perigee: | 305.2124° |
| revolutions per day: | 13.91751016 |
| mean anomaly at epoch: | 54.1338° |
| orbit number at epoch: | 93242 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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