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 55650U 26145.00889825 +.00000000 +00000-0 +46208-4 0 00006
2 55650 69.9993 352.0140 0002334 273.5800 86.5092 14.98332647 07
| Epoch (UTC): | 25 May 2026 00:12:48 |
| Eccentricity: | 0.0002334 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 352.0140° |
| argument of perigee: | 273.5800° |
| revolutions per day: | 14.98332647 |
| mean anomaly at epoch: | 86.5092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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