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 49730U 26145.50166689 +.00000000 +00000-0 -61343-4 0 00007
2 49730 53.2123 174.4900 0001231 79.1001 281.0130 15.08845650 08
| Epoch (UTC): | 25 May 2026 12:02:24 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 174.4900° |
| argument of perigee: | 79.1001° |
| revolutions per day: | 15.08845650 |
| mean anomaly at epoch: | 281.0130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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