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 39190U 26145.43741514 +.00000000 +00000-0 +00000-0 0 00002
2 39190 0.0413 339.6225 0002763 80.6032 299.8013 5.00116014 09
| Epoch (UTC): | 25 May 2026 10:29:52 |
| Eccentricity: | 0.0002763 |
| inclination: | 0.0413° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 339.6225° |
| argument of perigee: | 80.6032° |
| revolutions per day: | 5.00116014 |
| mean anomaly at epoch: | 299.8013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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