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 65676U 26145.28305709 +.00000000 +00000-0 +55690-3 0 00003
2 65676 53.1612 349.6696 0001337 86.4193 273.6961 15.30211923 09
| Epoch (UTC): | 25 May 2026 06:47:36 |
| Eccentricity: | 0.0001337 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.6696° |
| argument of perigee: | 86.4193° |
| revolutions per day: | 15.30211923 |
| mean anomaly at epoch: | 273.6961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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