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 65423U 26145.41527425 +.00000000 +00000-0 +37064-3 0 00004
2 65423 53.1583 235.8028 0001110 113.9957 246.1161 15.31716457 04
| Epoch (UTC): | 25 May 2026 09:57:59 |
| Eccentricity: | 0.0001110 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.8028° |
| argument of perigee: | 113.9957° |
| revolutions per day: | 15.31716457 |
| mean anomaly at epoch: | 246.1161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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