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 65743U 26144.81580095 +.00000000 +00000-0 +52153-3 0 00000
2 65743 53.1602 338.9496 0000853 107.4156 252.6938 15.30213573 01
| Epoch (UTC): | 24 May 2026 19:34:45 |
| Eccentricity: | 0.0000853 |
| inclination: | 53.1602° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.9496° |
| argument of perigee: | 107.4156° |
| revolutions per day: | 15.30213573 |
| mean anomaly at epoch: | 252.6938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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