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 39285U 26145.58936178 +.00000000 +00000-0 +00000-0 0 00005
2 39285 0.0714 317.4635 0002602 111.8010 54.6026 1.00273040 02
| Epoch (UTC): | 25 May 2026 14:08:40 |
| Eccentricity: | 0.0002602 |
| inclination: | 0.0714° |
| perigee height: | 35775 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 317.4635° |
| argument of perigee: | 111.8010° |
| revolutions per day: | 1.00273040 |
| mean anomaly at epoch: | 54.6026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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