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 39076U 26145.55491155 +.00000000 +00000-0 -63209-3 0 00005
2 39076 51.9896 352.5300 0000784 164.5656 195.5235 12.62259806 06
| Epoch (UTC): | 25 May 2026 13:19:04 |
| Eccentricity: | 0.0000784 |
| inclination: | 51.9896° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 352.5300° |
| argument of perigee: | 164.5656° |
| revolutions per day: | 12.62259806 |
| mean anomaly at epoch: | 195.5235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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