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 43602U 26144.28284340 +.00000000 +00000-0 +00000-0 0 00006
2 43602 54.1791 181.8510 0007779 30.2121 329.8983 1.86227821 06
| Epoch (UTC): | 24 May 2026 06:47:17 |
| Eccentricity: | 0.0007779 |
| inclination: | 54.1791° |
| perigee height: | 21507 km |
| apogee height: | 21550 km |
| right ascension of ascending node: | 181.8510° |
| argument of perigee: | 30.2121° |
| revolutions per day: | 1.86227821 |
| mean anomaly at epoch: | 329.8983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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