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 38666U 26084.83851236 +.00000000 +00000-0 +64191-4 0 00003
2 38666 74.0455 119.3347 0028512 271.0034 88.7853 14.37805144 05
| Epoch (UTC): | 25 March 2026 20:07:27 |
| Eccentricity: | 0.0028512 |
| inclination: | 74.0455° |
| perigee height: | 745 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 119.3347° |
| argument of perigee: | 271.0034° |
| revolutions per day: | 14.37805144 |
| mean anomaly at epoch: | 88.7853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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