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 65206U 26145.40272749 +.00000000 +00000-0 +59062-3 0 00000
2 65206 53.1579 155.8304 0000946 94.8677 265.2434 15.34400220 04
| Epoch (UTC): | 25 May 2026 09:39:55 |
| Eccentricity: | 0.0000946 |
| inclination: | 53.1579° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.8304° |
| argument of perigee: | 94.8677° |
| revolutions per day: | 15.34400220 |
| mean anomaly at epoch: | 265.2434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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