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 65741U 26145.25412166 +.00000000 +00000-0 +91091-3 0 00004
2 65741 53.1625 337.4266 0000247 121.3871 238.7154 15.30217545 07
| Epoch (UTC): | 25 May 2026 06:05:56 |
| Eccentricity: | 0.0000247 |
| inclination: | 53.1625° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 337.4266° |
| argument of perigee: | 121.3871° |
| revolutions per day: | 15.30217545 |
| mean anomaly at epoch: | 238.7154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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