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 26145.14329324 +.00000000 +00000-0 +31850-3 0 00003
2 39417 97.8108 107.3549 0040393 329.4960 30.3915 15.00987824 05
| Epoch (UTC): | 25 May 2026 03:26:20 |
| Eccentricity: | 0.0040393 |
| inclination: | 97.8108° |
| perigee height: | 536 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 107.3549° |
| argument of perigee: | 329.4960° |
| revolutions per day: | 15.00987824 |
| mean anomaly at epoch: | 30.3915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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