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 49450U 26145.53293666 +.00000000 +00000-0 +37641-3 0 00007
2 49450 53.2142 234.1954 0001291 81.5066 278.6073 15.08839697 07
| Epoch (UTC): | 25 May 2026 12:47:25 |
| Eccentricity: | 0.0001291 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.1954° |
| argument of perigee: | 81.5066° |
| revolutions per day: | 15.08839697 |
| mean anomaly at epoch: | 278.6073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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