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 39079U 26145.45023351 +.00000000 +00000-0 +00000-0 0 00002
2 39079 0.0331 84.5401 0001177 0.7696 5.7960 1.00272293 06
| Epoch (UTC): | 25 May 2026 10:48:20 |
| Eccentricity: | 0.0001177 |
| inclination: | 0.0331° |
| perigee height: | 35781 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 84.5401° |
| argument of perigee: | 0.7696° |
| revolutions per day: | 1.00272293 |
| mean anomaly at epoch: | 5.7960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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