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 39202U 26145.65177839 +.00000000 +00000-0 +80275-4 0 00009
2 39202 98.2864 330.3081 0008951 311.4623 48.5810 14.64860613 01
| Epoch (UTC): | 25 May 2026 15:38:33 |
| Eccentricity: | 0.0008951 |
| inclination: | 98.2864° |
| perigee height: | 671 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 330.3081° |
| argument of perigee: | 311.4623° |
| revolutions per day: | 14.64860613 |
| mean anomaly at epoch: | 48.5810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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