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 55374U 26145.34860448 +.00000000 +00000-0 +18417-4 0 00007
2 55374 43.0031 248.9058 0002018 279.6996 80.3628 15.27574954 08
| Epoch (UTC): | 25 May 2026 08:21:59 |
| Eccentricity: | 0.0002018 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 248.9058° |
| argument of perigee: | 279.6996° |
| revolutions per day: | 15.27574954 |
| mean anomaly at epoch: | 80.3628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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