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 65376U 26145.39124501 +.00000000 +00000-0 +86963-3 0 00008
2 65376 53.1588 171.5366 0001153 51.2079 308.9027 15.34410055 09
| Epoch (UTC): | 25 May 2026 09:23:23 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 171.5366° |
| argument of perigee: | 51.2079° |
| revolutions per day: | 15.34410055 |
| mean anomaly at epoch: | 308.9027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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