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 25994U 99068A 16274.22214339 -.00000055 00000-0 -21075-5 0 9999
2 25994 98.2039 347.0036 0001378 86.2606 273.8755 14.57110505892816
| Epoch (UTC): | 30 September 2016 05:19:53 |
| Eccentricity: | 0.0001378 |
| inclination: | 98.2039° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 347.0036° |
| argument of perigee: | 86.2606° |
| revolutions per day: | 14.57110505 |
| mean anomaly at epoch: | 273.8755° |
| orbit number at epoch: | 89281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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