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 65125U 26145.64063345 +.00000000 +00000-0 +19675-3 0 00002
2 65125 49.9928 278.7831 0017913 326.5011 33.4794 14.83936705 03
| Epoch (UTC): | 25 May 2026 15:22:30 |
| Eccentricity: | 0.0017913 |
| inclination: | 49.9928° |
| perigee height: | 604 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 278.7831° |
| argument of perigee: | 326.5011° |
| revolutions per day: | 14.83936705 |
| mean anomaly at epoch: | 33.4794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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