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 40921U 26145.56808521 +.00000000 +00000-0 +83227-3 0 00007
2 40921 82.4858 92.2650 0015556 72.8514 287.4267 12.42913723 06
| Epoch (UTC): | 25 May 2026 13:38:02 |
| Eccentricity: | 0.0015556 |
| inclination: | 82.4858° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 92.2650° |
| argument of perigee: | 72.8514° |
| revolutions per day: | 12.42913723 |
| mean anomaly at epoch: | 287.4267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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