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 41240U 26152.54632931 +.00000000 +00000-0 +45048-4 0 00008
2 41240 66.0389 158.7188 0008599 273.3348 86.6687 12.87627701 06
| Epoch (UTC): | 01 June 2026 13:06:42 |
| Eccentricity: | 0.0008599 |
| inclination: | 66.0389° |
| perigee height: | 1304 km |
| apogee height: | 1318 km |
| right ascension of ascending node: | 158.7188° |
| argument of perigee: | 273.3348° |
| revolutions per day: | 12.87627701 |
| mean anomaly at epoch: | 86.6687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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