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 43662U 26145.59138433 +.00000000 +00000-0 +15390-3 0 00009
2 43662 97.3609 150.7894 0001189 66.5569 293.5790 15.16539272 03
| Epoch (UTC): | 25 May 2026 14:11:35 |
| Eccentricity: | 0.0001189 |
| inclination: | 97.3609° |
| perigee height: | 515 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 150.7894° |
| argument of perigee: | 66.5569° |
| revolutions per day: | 15.16539272 |
| mean anomaly at epoch: | 293.5790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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