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 57622U 26145.62975875 +.00000000 +00000-0 +70845-4 0 00000
2 57622 43.0015 7.0154 0001081 279.3190 80.7539 15.27571037 05
| Epoch (UTC): | 25 May 2026 15:06:51 |
| Eccentricity: | 0.0001081 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.0154° |
| argument of perigee: | 279.3190° |
| revolutions per day: | 15.27571037 |
| mean anomaly at epoch: | 80.7539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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