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 26635U 00080A 18096.24969320 0.00000000 00000-0 00000-0 0 02
2 26635 8.2712 34.4469 0007383 197.3381 162.6485 1.00270000 09
| Epoch (UTC): | 06 April 2018 05:59:33 |
| Eccentricity: | 0.0007383 |
| inclination: | 8.2712° |
| perigee height: | 35755 km |
| apogee height: | 35818 km |
| right ascension of ascending node: | 34.4469° |
| argument of perigee: | 197.3381° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 162.6485° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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