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 65842U 26145.27406834 +.00000000 +00000-0 +88913-3 0 00002
2 65842 53.1589 92.2732 0001117 94.1164 265.9967 15.34419139 02
| Epoch (UTC): | 25 May 2026 06:34:39 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.2732° |
| argument of perigee: | 94.1164° |
| revolutions per day: | 15.34419139 |
| mean anomaly at epoch: | 265.9967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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