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 44905U 26145.58915566 +.00000000 +00000-0 +12974-2 0 00003
2 44905 82.5214 98.6493 0012537 197.9412 162.1226 12.42869644 02
| Epoch (UTC): | 25 May 2026 14:08:23 |
| Eccentricity: | 0.0012537 |
| inclination: | 82.5214° |
| perigee height: | 1485 km |
| apogee height: | 1504 km |
| right ascension of ascending node: | 98.6493° |
| argument of perigee: | 197.9412° |
| revolutions per day: | 12.42869644 |
| mean anomaly at epoch: | 162.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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