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 65936U 26145.23309556 +.00000000 +00000-0 +39552-3 0 00000
2 65936 53.1577 170.3969 0001207 90.8580 269.2559 15.30206123 05
| Epoch (UTC): | 25 May 2026 05:35:39 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 170.3969° |
| argument of perigee: | 90.8580° |
| revolutions per day: | 15.30206123 |
| mean anomaly at epoch: | 269.2559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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