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 14209.50958468 .00000124 00000-0 37685-4 0 4739
2 25994 098.2103 283.6724 0001280 097.3025 262.8330 14.57088656777086
| Epoch (UTC): | 28 July 2014 12:13:48 |
| Eccentricity: | 0.0001280 |
| inclination: | 98.2103° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 283.6724° |
| argument of perigee: | 97.3025° |
| revolutions per day: | 14.57088656 |
| mean anomaly at epoch: | 262.8330° |
| orbit number at epoch: | 77708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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