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 38741U 26145.56934169 +.00000000 +00000-0 +00000-0 0 00007
2 38741 2.3712 81.3328 0002888 4.7488 289.4735 1.00271087 06
| Epoch (UTC): | 25 May 2026 13:39:51 |
| Eccentricity: | 0.0002888 |
| inclination: | 2.3712° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 81.3328° |
| argument of perigee: | 4.7488° |
| revolutions per day: | 1.00271087 |
| mean anomaly at epoch: | 289.4735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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