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 39640U 26087.09940860 +.00000000 +00000-0 +15129-3 0 00005
2 39640 65.0087 231.7370 0016453 282.1220 77.8023 14.34205275 09
| Epoch (UTC): | 28 March 2026 02:23:08 |
| Eccentricity: | 0.0016453 |
| inclination: | 65.0087° |
| perigee height: | 766 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 231.7370° |
| argument of perigee: | 282.1220° |
| revolutions per day: | 14.34205275 |
| mean anomaly at epoch: | 77.8023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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