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 49444U 26145.52008703 +.00000000 +00000-0 +33808-4 0 00007
2 49444 53.2108 224.2263 0001251 83.4792 276.6342 15.08835598 01
| Epoch (UTC): | 25 May 2026 12:28:55 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.2263° |
| argument of perigee: | 83.4792° |
| revolutions per day: | 15.08835598 |
| mean anomaly at epoch: | 276.6342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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