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 65761U 26144.92966058 +.00000000 +00000-0 +94086-3 0 00000
2 65761 53.1623 338.9479 0001005 77.0006 283.1107 15.30209074 09
| Epoch (UTC): | 24 May 2026 22:18:42 |
| Eccentricity: | 0.0001005 |
| inclination: | 53.1623° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.9479° |
| argument of perigee: | 77.0006° |
| revolutions per day: | 15.30209074 |
| mean anomaly at epoch: | 283.1107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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