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 66374U 26145.50131168 +.00000000 +00000-0 +56124-3 0 00003
2 66374 53.1622 232.9378 0000441 176.2539 183.8465 15.30196258 08
| Epoch (UTC): | 25 May 2026 12:01:53 |
| Eccentricity: | 0.0000441 |
| inclination: | 53.1622° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.9378° |
| argument of perigee: | 176.2539° |
| revolutions per day: | 15.30196258 |
| mean anomaly at epoch: | 183.8465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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