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 65095U 26145.58335647 +.00000000 +00000-0 +15010-2 0 00006
2 65095 53.1593 26.9853 0001019 88.2464 66.0570 15.42123134 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.1593° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 26.9853° |
| argument of perigee: | 88.2464° |
| revolutions per day: | 15.42123134 |
| mean anomaly at epoch: | 66.0570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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