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 17175.27784716 -.00000068 +00000-0 -50761-5 0 9994
2 25994 098.2080 250.2224 0001176 066.3501 293.7809 14.57113570931703
| Epoch (UTC): | 24 June 2017 06:40:05 |
| Eccentricity: | 0.0001176 |
| inclination: | 98.2080° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 250.2224° |
| argument of perigee: | 66.3501° |
| revolutions per day: | 14.57113570 |
| mean anomaly at epoch: | 293.7809° |
| orbit number at epoch: | 93170 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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