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 25336U 98029A 18248.10420977 0.00000000 00000-0 00000-0 0 03
2 25336 8.8660 355.2778 0039254 270.6570 88.8996 1.00270000 04
| Epoch (UTC): | 05 September 2018 02:30:03 |
| Eccentricity: | 0.0039254 |
| inclination: | 8.8660° |
| perigee height: | 35621 km |
| apogee height: | 35952 km |
| right ascension of ascending node: | 355.2778° |
| argument of perigee: | 270.6570° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 88.8996° |
| 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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