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 43445U 26145.14664191 +.00000000 +00000-0 +00000-0 0 00003
2 43445 7.0640 67.2269 0010716 168.4910 12.4002 1.02112913 04
| Epoch (UTC): | 25 May 2026 03:31:09 |
| Eccentricity: | 0.0010716 |
| inclination: | 7.0640° |
| perigee height: | 35234 km |
| apogee height: | 35323 km |
| right ascension of ascending node: | 67.2269° |
| argument of perigee: | 168.4910° |
| revolutions per day: | 1.02112913 |
| mean anomaly at epoch: | 12.4002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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