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 61639U 26145.50535955 +.00000000 +00000-0 +59889-4 0 00006
2 61639 42.9993 80.7471 0000691 255.5447 104.5328 15.27570810 07
| Epoch (UTC): | 25 May 2026 12:07:43 |
| Eccentricity: | 0.0000691 |
| inclination: | 42.9993° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.7471° |
| argument of perigee: | 255.5447° |
| revolutions per day: | 15.27570810 |
| mean anomaly at epoch: | 104.5328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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