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 49742U 26145.46944801 +.00000000 +00000-0 +30357-5 0 00006
2 49742 53.2125 164.4422 0001235 74.7463 285.3665 15.08835829 05
| Epoch (UTC): | 25 May 2026 11:16:00 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.4422° |
| argument of perigee: | 74.7463° |
| revolutions per day: | 15.08835829 |
| mean anomaly at epoch: | 285.3665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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