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 44476U 26145.59577514 +.00000000 +00000-0 +00000-0 0 00009
2 44476 0.0157 311.5451 0000520 16.9758 191.0831 1.00271578 07
| Epoch (UTC): | 25 May 2026 14:17:54 |
| Eccentricity: | 0.0000520 |
| inclination: | 0.0157° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 311.5451° |
| argument of perigee: | 16.9758° |
| revolutions per day: | 1.00271578 |
| mean anomaly at epoch: | 191.0831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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