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 56039U 26145.54641742 +.00000000 +00000-0 +35310-4 0 00003
2 56039 43.0057 316.9334 0001697 273.1884 86.8773 15.27579058 07
| Epoch (UTC): | 25 May 2026 13:06:50 |
| Eccentricity: | 0.0001697 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9334° |
| argument of perigee: | 273.1884° |
| revolutions per day: | 15.27579058 |
| mean anomaly at epoch: | 86.8773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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