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 39487U 26145.32626986 +.00000000 +00000-0 +00000-0 0 00004
2 39487 0.0176 291.9569 0001224 37.6640 170.7914 1.00272281 05
| Epoch (UTC): | 25 May 2026 07:49:49 |
| Eccentricity: | 0.0001224 |
| inclination: | 0.0176° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 291.9569° |
| argument of perigee: | 37.6640° |
| revolutions per day: | 1.00272281 |
| mean anomaly at epoch: | 170.7914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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