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 65754U 26145.26983979 +.00000000 +00000-0 +84606-3 0 00008
2 65754 53.1602 336.8057 0001409 73.3426 286.7729 15.30209133 05
| Epoch (UTC): | 25 May 2026 06:28:34 |
| Eccentricity: | 0.0001409 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.8057° |
| argument of perigee: | 73.3426° |
| revolutions per day: | 15.30209133 |
| mean anomaly at epoch: | 286.7729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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