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 49438U 26145.59000002 +.00000000 +00000-0 +34856-4 0 00005
2 49438 53.2125 223.8378 0001261 83.6672 276.4464 15.08834654 00
| Epoch (UTC): | 25 May 2026 14:09:36 |
| Eccentricity: | 0.0001261 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 223.8378° |
| argument of perigee: | 83.6672° |
| revolutions per day: | 15.08834654 |
| mean anomaly at epoch: | 276.4464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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