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 is defined by the following mean orbital elements,
1 25039U 97069A 18042.52217099 .30422284 -12919-5 23927-3 0 9999
2 25039 86.3528 257.4987 0011688 182.9697 178.7481 16.52305555 63968
| Epoch (UTC): | 11 February 2018 12:31:55 |
| Eccentricity: | 0.0011688 |
| inclination: | 86.3528° |
| perigee height: | 125 km |
| apogee height: | 141 km |
| right ascension of ascending node: | 257.4987° |
| argument of perigee: | 182.9697° |
| revolutions per day: | 16.52305555 |
| mean anomaly at epoch: | 178.7481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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