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 44449U 26145.31745317 +.00000000 +00000-0 +15852-3 0 00001
2 44449 34.9925 109.4706 0002711 76.2111 283.8899 15.02519739 04
| Epoch (UTC): | 25 May 2026 07:37:07 |
| Eccentricity: | 0.0002711 |
| inclination: | 34.9925° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 109.4706° |
| argument of perigee: | 76.2111° |
| revolutions per day: | 15.02519739 |
| mean anomaly at epoch: | 283.8899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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