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 25134U 98002A 18344.39379586 -.00000243 00000-0 00000+0 0 9993
2 25134 10.9989 27.2647 0000246 227.7672 132.2305 0.99156785 76218
| Epoch (UTC): | 10 December 2018 09:27:03 |
| Eccentricity: | 0.0000246 |
| inclination: | 10.9989° |
| perigee height: | 36100 km |
| apogee height: | 36103 km |
| right ascension of ascending node: | 27.2647° |
| argument of perigee: | 227.7672° |
| revolutions per day: | 0.99156785 |
| mean anomaly at epoch: | 132.2305° |
| orbit number at epoch: | 7621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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