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 115U 60002D 19339.47846918 -.00000077 00000-0 18016-4 0 9992
2 115 48.1654 131.7362 0034257 110.2909 250.1691 14.83515072184028
| Epoch (UTC): | 05 December 2019 11:28:59 |
| Eccentricity: | 0.0034257 |
| inclination: | 48.1654° |
| perigee height: | 594 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 131.7362° |
| argument of perigee: | 110.2909° |
| revolutions per day: | 14.83515072 |
| mean anomaly at epoch: | 250.1691° |
| orbit number at epoch: | 18402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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