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 26073.57141022 +.00000000 +00000-0 +12835-3 0 00005
2 37839 19.9595 163.2385 0018726 111.0167 277.7923 14.13743579 00
| Epoch (UTC): | 14 March 2026 13:42:49 |
| Eccentricity: | 0.0018726 |
| inclination: | 19.9595° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 163.2385° |
| argument of perigee: | 111.0167° |
| revolutions per day: | 14.13743579 |
| mean anomaly at epoch: | 277.7923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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