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 26074.93735352 +.00000000 +00000-0 +98254-4 0 00001
2 37839 19.9595 154.9394 0018674 126.0702 29.7567 14.13743819 06
| Epoch (UTC): | 15 March 2026 22:29:47 |
| Eccentricity: | 0.0018674 |
| inclination: | 19.9595° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 154.9394° |
| argument of perigee: | 126.0702° |
| revolutions per day: | 14.13743819 |
| mean anomaly at epoch: | 29.7567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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