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 65745U 26145.52793463 +.00000000 +00000-0 +92877-3 0 00003
2 65745 53.1610 335.5750 0001606 85.3569 274.7615 15.30216551 03
| Epoch (UTC): | 25 May 2026 12:40:13 |
| Eccentricity: | 0.0001606 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.5750° |
| argument of perigee: | 85.3569° |
| revolutions per day: | 15.30216551 |
| mean anomaly at epoch: | 274.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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