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 37839U 26145.51765956 +.00000000 +00000-0 +74348-4 0 00005
2 37839 19.9607 86.1454 0018606 185.5391 330.0267 14.13769201 00
| Epoch (UTC): | 25 May 2026 12:25:25 |
| Eccentricity: | 0.0018606 |
| inclination: | 19.9607° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 86.1454° |
| argument of perigee: | 185.5391° |
| revolutions per day: | 14.13769201 |
| mean anomaly at epoch: | 330.0267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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