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 65082U 26145.38349705 +.00000000 +00000-0 +15185-2 0 00003
2 65082 53.1592 27.5514 0001688 91.0459 269.0741 15.42177812 00
| Epoch (UTC): | 25 May 2026 09:12:14 |
| Eccentricity: | 0.0001688 |
| inclination: | 53.1592° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 27.5514° |
| argument of perigee: | 91.0459° |
| revolutions per day: | 15.42177812 |
| mean anomaly at epoch: | 269.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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