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 65735U 26144.95381698 +.00000000 +00000-0 +62240-3 0 00002
2 65735 53.1598 338.3926 0000986 89.2953 270.8160 15.30213986 04
| Epoch (UTC): | 24 May 2026 22:53:29 |
| Eccentricity: | 0.0000986 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.3926° |
| argument of perigee: | 89.2953° |
| revolutions per day: | 15.30213986 |
| mean anomaly at epoch: | 270.8160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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