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 65902U 26145.06197515 +.00000000 +00000-0 +94605-3 0 00004
2 65902 53.1593 16.8544 0001204 83.7444 276.3694 15.30203277 02
| Epoch (UTC): | 25 May 2026 01:29:14 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 16.8544° |
| argument of perigee: | 83.7444° |
| revolutions per day: | 15.30203277 |
| mean anomaly at epoch: | 276.3694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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