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 49410U 26145.55872617 +.00000000 +00000-0 -20864-4 0 00005
2 49410 53.2129 244.0505 0001526 88.8125 271.3042 15.08839345 03
| Epoch (UTC): | 25 May 2026 13:24:33 |
| Eccentricity: | 0.0001526 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 244.0505° |
| argument of perigee: | 88.8125° |
| revolutions per day: | 15.08839345 |
| mean anomaly at epoch: | 271.3042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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