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 65904U 26073.04182464 +.00000000 +00000-0 +75498-3 0 00000
2 65904 53.1604 350.9135 0001166 116.5079 243.6042 15.30200308 07
| Epoch (UTC): | 14 March 2026 01:00:13 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.9135° |
| argument of perigee: | 116.5079° |
| revolutions per day: | 15.30200308 |
| mean anomaly at epoch: | 243.6042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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