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 65354U 26145.35556441 +.00000000 +00000-0 +55114-3 0 00006
2 65354 53.1589 172.0384 0001002 61.2970 298.8133 15.34411067 05
| Epoch (UTC): | 25 May 2026 08:32:00 |
| Eccentricity: | 0.0001002 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 172.0384° |
| argument of perigee: | 61.2970° |
| revolutions per day: | 15.34411067 |
| mean anomaly at epoch: | 298.8133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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