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 38977U 26145.01016345 +.00000000 +00000-0 +00000-0 0 00005
2 38977 10.4363 50.1131 0001291 157.1399 22.6486 1.00270191 01
| Epoch (UTC): | 25 May 2026 00:14:38 |
| Eccentricity: | 0.0001291 |
| inclination: | 10.4363° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 50.1131° |
| argument of perigee: | 157.1399° |
| revolutions per day: | 1.00270191 |
| mean anomaly at epoch: | 22.6486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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