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 65263U 26145.63444883 +.00000000 +00000-0 +12595-3 0 00008
2 65263 97.4782 273.0158 0001660 90.5025 269.6398 15.16346526 03
| Epoch (UTC): | 25 May 2026 15:13:36 |
| Eccentricity: | 0.0001660 |
| inclination: | 97.4782° |
| perigee height: | 516 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 273.0158° |
| argument of perigee: | 90.5025° |
| revolutions per day: | 15.16346526 |
| mean anomaly at epoch: | 269.6398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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