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 39416U 26145.14331029 +.00000000 +00000-0 +11761-3 0 00006
2 39416 97.7696 98.6973 0034349 288.7157 71.0335 14.91503708 09
| Epoch (UTC): | 25 May 2026 03:26:22 |
| Eccentricity: | 0.0034349 |
| inclination: | 97.7696° |
| perigee height: | 569 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 98.6973° |
| argument of perigee: | 288.7157° |
| revolutions per day: | 14.91503708 |
| mean anomaly at epoch: | 71.0335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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