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 65209U 26145.46576031 +.00000000 +00000-0 +83951-3 0 00004
2 65209 53.1570 155.5155 0001279 52.0806 308.0312 15.34410179 04
| Epoch (UTC): | 25 May 2026 11:10:41 |
| Eccentricity: | 0.0001279 |
| inclination: | 53.1570° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.5155° |
| argument of perigee: | 52.0806° |
| revolutions per day: | 15.34410179 |
| mean anomaly at epoch: | 308.0312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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