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 35869U 09049E 19341.50090220 .00000001 00000-0 19156-4 0 9996
2 35869 98.4197 330.9670 0005239 39.6542 320.5019 14.22423712530586
| Epoch (UTC): | 07 December 2019 12:01:17 |
| Eccentricity: | 0.0005239 |
| inclination: | 98.4197° |
| perigee height: | 813 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 330.9670° |
| argument of perigee: | 39.6542° |
| revolutions per day: | 14.22423712 |
| mean anomaly at epoch: | 320.5019° |
| orbit number at epoch: | 53058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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