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 65196U 26145.38118692 +.00000000 +00000-0 +17275-3 0 00001
2 65196 97.4508 17.9224 0002929 84.9757 275.1804 15.05658057 08
| Epoch (UTC): | 25 May 2026 09:08:54 |
| Eccentricity: | 0.0002929 |
| inclination: | 97.4508° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 17.9224° |
| argument of perigee: | 84.9757° |
| revolutions per day: | 15.05658057 |
| mean anomaly at epoch: | 275.1804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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