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 39017U 26145.60106109 +.00000000 +00000-0 +00000-0 0 00004
2 39017 0.0482 106.4101 0002994 311.9492 128.6977 1.00271370 03
| Epoch (UTC): | 25 May 2026 14:25:31 |
| Eccentricity: | 0.0002994 |
| inclination: | 0.0482° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 106.4101° |
| argument of perigee: | 311.9492° |
| revolutions per day: | 1.00271370 |
| mean anomaly at epoch: | 128.6977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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