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 39616U 26145.56908169 +.00000000 +00000-0 +00000-0 0 00000
2 39616 0.0581 156.8571 0003269 290.9483 286.2220 1.00272912 05
| Epoch (UTC): | 25 May 2026 13:39:28 |
| Eccentricity: | 0.0003269 |
| inclination: | 0.0581° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 156.8571° |
| argument of perigee: | 290.9483° |
| revolutions per day: | 1.00272912 |
| mean anomaly at epoch: | 286.2220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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