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 65755U 26145.53848486 +.00000000 +00000-0 +72749-3 0 00007
2 65755 53.1592 335.6335 0000801 119.7481 240.3600 15.30211689 04
| Epoch (UTC): | 25 May 2026 12:55:25 |
| Eccentricity: | 0.0000801 |
| inclination: | 53.1592° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.6335° |
| argument of perigee: | 119.7481° |
| revolutions per day: | 15.30211689 |
| mean anomaly at epoch: | 240.3600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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