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 61923U 26145.49803885 +.00000000 +00000-0 +42304-3 0 00003
2 61923 43.0043 211.8823 0001448 272.0362 88.0324 15.27589508 06
| Epoch (UTC): | 25 May 2026 11:57:10 |
| Eccentricity: | 0.0001448 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.8823° |
| argument of perigee: | 272.0362° |
| revolutions per day: | 15.27589508 |
| mean anomaly at epoch: | 88.0324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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