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 26110.85682750 +.00000000 +00000-0 +72841-4 0 00000
2 37839 19.9616 296.7276 0018553 163.2722 321.4985 14.13758469 08
| Epoch (UTC): | 20 April 2026 20:33:49 |
| Eccentricity: | 0.0018553 |
| inclination: | 19.9616° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 296.7276° |
| argument of perigee: | 163.2722° |
| revolutions per day: | 14.13758469 |
| mean anomaly at epoch: | 321.4985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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