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 65036U 26145.15128874 +.00000000 +00000-0 +50719-3 0 00002
2 65036 53.1587 299.2444 0002290 73.3064 286.8188 15.30207759 01
| Epoch (UTC): | 25 May 2026 03:37:51 |
| Eccentricity: | 0.0002290 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 299.2444° |
| argument of perigee: | 73.3064° |
| revolutions per day: | 15.30207759 |
| mean anomaly at epoch: | 286.8188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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