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 39008U 26141.18701858 +.00000000 +00000-0 +00000-0 0 00005
2 39008 0.0110 320.0233 0001991 105.4260 179.2055 1.00271273 07
| Epoch (UTC): | 21 May 2026 04:29:18 |
| Eccentricity: | 0.0001991 |
| inclination: | 0.0110° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 320.0233° |
| argument of perigee: | 105.4260° |
| revolutions per day: | 1.00271273 |
| mean anomaly at epoch: | 179.2055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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