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 39216U 26145.60944615 +.00000000 +00000-0 +00000-0 0 00007
2 39216 1.8700 82.8085 0000851 319.7935 189.5022 1.00273815 05
| Epoch (UTC): | 25 May 2026 14:37:36 |
| Eccentricity: | 0.0000851 |
| inclination: | 1.8700° |
| perigee height: | 35782 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 82.8085° |
| argument of perigee: | 319.7935° |
| revolutions per day: | 1.00273815 |
| mean anomaly at epoch: | 189.5022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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