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 65506U 26145.64099795 +.00000000 +00000-0 +87155-3 0 00001
2 65506 53.1596 272.7207 0001759 99.5428 260.5774 15.34406929 03
| Epoch (UTC): | 25 May 2026 15:23:02 |
| Eccentricity: | 0.0001759 |
| inclination: | 53.1596° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 272.7207° |
| argument of perigee: | 99.5428° |
| revolutions per day: | 15.34406929 |
| mean anomaly at epoch: | 260.5774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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