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 26069.48634240 +.00000000 +00000-0 +13957-3 0 00005
2 37839 19.9594 188.0571 0018776 66.2458 6.6166 14.13741346 08
| Epoch (UTC): | 10 March 2026 11:40:19 |
| Eccentricity: | 0.0018776 |
| inclination: | 19.9594° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 188.0571° |
| argument of perigee: | 66.2458° |
| revolutions per day: | 14.13741346 |
| mean anomaly at epoch: | 6.6166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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