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 38098U 26145.38413727 +.00000000 +00000-0 +00000-0 0 00004
2 38098 0.0226 72.5869 0001720 349.8395 30.9535 1.00272523 05
| Epoch (UTC): | 25 May 2026 09:13:09 |
| Eccentricity: | 0.0001720 |
| inclination: | 0.0226° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 72.5869° |
| argument of perigee: | 349.8395° |
| revolutions per day: | 1.00272523 |
| mean anomaly at epoch: | 30.9535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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