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 26105.07725022 +.00000000 +00000-0 +68443-4 0 00001
2 37839 19.9623 331.8381 0018602 99.6952 65.9503 14.13757075 04
| Epoch (UTC): | 15 April 2026 01:51:14 |
| Eccentricity: | 0.0018602 |
| inclination: | 19.9623° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 331.8381° |
| argument of perigee: | 99.6952° |
| revolutions per day: | 14.13757075 |
| mean anomaly at epoch: | 65.9503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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