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 65090U 26145.41497308 +.00000000 +00000-0 +66310-3 0 00006
2 65090 53.1610 30.5029 0001287 110.3424 249.7715 15.30209960 00
| Epoch (UTC): | 25 May 2026 09:57:33 |
| Eccentricity: | 0.0001287 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.5029° |
| argument of perigee: | 110.3424° |
| revolutions per day: | 15.30209960 |
| mean anomaly at epoch: | 249.7715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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