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 44314U 26145.31176747 +.00000000 +00000-0 +50592-3 0 00007
2 44314 44.9993 106.6306 0007260 199.0513 161.0104 15.37826808 02
| Epoch (UTC): | 25 May 2026 07:28:56 |
| Eccentricity: | 0.0007260 |
| inclination: | 44.9993° |
| perigee height: | 448 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 106.6306° |
| argument of perigee: | 199.0513° |
| revolutions per day: | 15.37826808 |
| mean anomaly at epoch: | 161.0104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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