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 38752U 26069.80903477 +.00000000 +00000-0 +85947-3 0 00005
2 38752 9.5479 240.7241 0548826 299.3995 55.2519 15.26561984 04
| Epoch (UTC): | 10 March 2026 19:25:00 |
| Eccentricity: | 0.0548826 |
| inclination: | 9.5479° |
| perigee height: | 109 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 240.7241° |
| argument of perigee: | 299.3995° |
| revolutions per day: | 15.26561984 |
| mean anomaly at epoch: | 55.2519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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