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 25276U 98019E 16268.43425474 .00000148 00000-0 45623-4 0 9992
2 25276 86.3974 38.0920 0002135 96.2973 263.8466 14.34216048967976
| Epoch (UTC): | 24 September 2016 10:25:19 |
| Eccentricity: | 0.0002135 |
| inclination: | 86.3974° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 38.0920° |
| argument of perigee: | 96.2973° |
| revolutions per day: | 14.34216048 |
| mean anomaly at epoch: | 263.8466° |
| orbit number at epoch: | 96797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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