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 44479U 26145.58710845 +.00000000 +00000-0 +00000-0 0 00007
2 44479 0.0144 331.4337 0001410 97.1263 42.9708 1.00270022 01
| Epoch (UTC): | 25 May 2026 14:05:26 |
| Eccentricity: | 0.0001410 |
| inclination: | 0.0144° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 331.4337° |
| argument of perigee: | 97.1263° |
| revolutions per day: | 1.00270022 |
| mean anomaly at epoch: | 42.9708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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