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 65479U 26145.60353075 +.00000000 +00000-0 +86165-2 0 00009
2 65479 53.1576 260.6245 0001711 170.3597 189.7438 15.31564260 00
| Epoch (UTC): | 25 May 2026 14:29:05 |
| Eccentricity: | 0.0001711 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 260.6245° |
| argument of perigee: | 170.3597° |
| revolutions per day: | 15.31564260 |
| mean anomaly at epoch: | 189.7438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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