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 49737U 26145.44368748 +.00000000 +00000-0 +24818-4 0 00002
2 49737 53.2119 164.5583 0000928 70.9823 289.1270 15.08841296 06
| Epoch (UTC): | 25 May 2026 10:38:54 |
| Eccentricity: | 0.0000928 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.5583° |
| argument of perigee: | 70.9823° |
| revolutions per day: | 15.08841296 |
| mean anomaly at epoch: | 289.1270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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