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 39209U 26145.46680897 +.00000000 +00000-0 +13393-3 0 00004
2 39209 98.0817 151.7531 0003685 186.0424 174.0741 14.74559321 03
| Epoch (UTC): | 25 May 2026 11:12:12 |
| Eccentricity: | 0.0003685 |
| inclination: | 98.0817° |
| perigee height: | 644 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 151.7531° |
| argument of perigee: | 186.0424° |
| revolutions per day: | 14.74559321 |
| mean anomaly at epoch: | 174.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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