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 39508U 26145.52727177 +.00000000 +00000-0 +00000-0 0 00004
2 39508 0.0575 91.4194 0004010 326.8748 89.5649 1.00272099 06
| Epoch (UTC): | 25 May 2026 12:39:16 |
| Eccentricity: | 0.0004010 |
| inclination: | 0.0575° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 91.4194° |
| argument of perigee: | 326.8748° |
| revolutions per day: | 1.00272099 |
| mean anomaly at epoch: | 89.5649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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