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 65044U 26145.60393154 +.00000000 +00000-0 +63655-4 0 00000
2 65044 50.0020 346.8931 0000454 39.0416 321.0489 13.29323518 02
| Epoch (UTC): | 25 May 2026 14:29:39 |
| Eccentricity: | 0.0000454 |
| inclination: | 50.0020° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 346.8931° |
| argument of perigee: | 39.0416° |
| revolutions per day: | 13.29323518 |
| mean anomaly at epoch: | 321.0489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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