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 65026U 26145.13862396 +.00000000 +00000-0 +63339-3 0 00005
2 65026 53.1597 299.1647 0001686 85.3283 274.7910 15.30211393 07
| Epoch (UTC): | 25 May 2026 03:19:37 |
| Eccentricity: | 0.0001686 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 299.1647° |
| argument of perigee: | 85.3283° |
| revolutions per day: | 15.30211393 |
| mean anomaly at epoch: | 274.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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