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 38354U 26145.63575534 +.00000000 +00000-0 -64832-3 0 00009
2 38354 100.7380 349.9934 0025231 343.9625 16.0687 13.18381695 03
| Epoch (UTC): | 25 May 2026 15:15:29 |
| Eccentricity: | 0.0025231 |
| inclination: | 100.7380° |
| perigee height: | 1172 km |
| apogee height: | 1210 km |
| right ascension of ascending node: | 349.9934° |
| argument of perigee: | 343.9625° |
| revolutions per day: | 13.18381695 |
| mean anomaly at epoch: | 16.0687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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