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 38552U 26118.63307963 +.00000000 +00000-0 +00000-0 0 00001
2 38552 4.5569 61.2306 0002138 316.2681 67.1677 1.00268609 09
| Epoch (UTC): | 28 April 2026 15:11:38 |
| Eccentricity: | 0.0002138 |
| inclination: | 4.5569° |
| perigee height: | 35778 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 61.2306° |
| argument of perigee: | 316.2681° |
| revolutions per day: | 1.00268609 |
| mean anomaly at epoch: | 67.1677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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