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 55413U 26145.57520019 +.00000000 +00000-0 +26037-4 0 00000
2 55413 69.9993 250.4045 0003181 268.5556 91.5239 14.98326715 00
| Epoch (UTC): | 25 May 2026 13:48:17 |
| Eccentricity: | 0.0003181 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.4045° |
| argument of perigee: | 268.5556° |
| revolutions per day: | 14.98326715 |
| mean anomaly at epoch: | 91.5239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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