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 49772U 26145.22536802 +.00000000 +00000-0 +37860-3 0 00005
2 49772 53.1940 154.8245 0003382 12.8669 347.2428 15.52134128 02
| Epoch (UTC): | 25 May 2026 05:24:31 |
| Eccentricity: | 0.0003382 |
| inclination: | 53.1940° |
| perigee height: | 408 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 154.8245° |
| argument of perigee: | 12.8669° |
| revolutions per day: | 15.52134128 |
| mean anomaly at epoch: | 347.2428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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