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 38733U 26118.85354299 +.00000000 +00000-0 +12546-2 0 00000
2 38733 82.4699 105.9872 0018581 179.7195 180.3898 12.42434621 04
| Epoch (UTC): | 28 April 2026 20:29:06 |
| Eccentricity: | 0.0018581 |
| inclination: | 82.4699° |
| perigee height: | 1482 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 105.9872° |
| argument of perigee: | 179.7195° |
| revolutions per day: | 12.42434621 |
| mean anomaly at epoch: | 180.3898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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