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 39417U 26106.47430911 +.00000000 +00000-0 +19290-3 0 00005
2 39417 97.8130 68.4832 0044892 98.0747 262.5573 15.00673871 05
| Epoch (UTC): | 16 April 2026 11:23:00 |
| Eccentricity: | 0.0044892 |
| inclination: | 97.8130° |
| perigee height: | 534 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 68.4832° |
| argument of perigee: | 98.0747° |
| revolutions per day: | 15.00673871 |
| mean anomaly at epoch: | 262.5573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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