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 38735U 26039.13286799 +.00000000 +00000-0 +22903-3 0 00003
2 38735 82.4795 155.1664 0016776 351.8024 8.2779 12.42643243 05
| Epoch (UTC): | 08 February 2026 03:11:19 |
| Eccentricity: | 0.0016776 |
| inclination: | 82.4795° |
| perigee height: | 1482 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 155.1664° |
| argument of perigee: | 351.8024° |
| revolutions per day: | 12.42643243 |
| mean anomaly at epoch: | 8.2779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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