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 65102U 26145.39681366 +.00000000 +00000-0 +10433-2 0 00000
2 65102 53.1606 27.5451 0001060 88.8563 271.2564 15.42196499 03
| Epoch (UTC): | 25 May 2026 09:31:24 |
| Eccentricity: | 0.0001060 |
| inclination: | 53.1606° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 27.5451° |
| argument of perigee: | 88.8563° |
| revolutions per day: | 15.42196499 |
| mean anomaly at epoch: | 271.2564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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