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 35008U 09029A 17172.25798072 -.00000033 +00000-0 +14674-2 0 9995
2 35008 064.6248 043.6914 7181563 255.2336 344.7369 02.24471866066156
| Epoch (UTC): | 21 June 2017 06:11:29 |
| Eccentricity: | 0.7181563 |
| inclination: | 64.6248° |
| perigee height: | 566 km |
| apogee height: | 35955 km |
| right ascension of ascending node: | 43.6914° |
| argument of perigee: | 255.2336° |
| revolutions per day: | 2.24471866 |
| mean anomaly at epoch: | 344.7369° |
| orbit number at epoch: | 6615 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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