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 65374U 26145.47802369 +.00000000 +00000-0 +54748-3 0 00006
2 65374 53.1587 171.3712 0001058 66.8347 293.2765 15.30208714 01
| Epoch (UTC): | 25 May 2026 11:28:21 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.3712° |
| argument of perigee: | 66.8347° |
| revolutions per day: | 15.30208714 |
| mean anomaly at epoch: | 293.2765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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