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 66241U 26145.65374641 +.00000000 +00000-0 +50038-3 0 00005
2 66241 53.1613 286.1495 0000335 78.7383 281.3655 15.30194051 01
| Epoch (UTC): | 25 May 2026 15:41:23 |
| Eccentricity: | 0.0000335 |
| inclination: | 53.1613° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 286.1495° |
| argument of perigee: | 78.7383° |
| revolutions per day: | 15.30194051 |
| mean anomaly at epoch: | 281.3655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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