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 40970U 26145.57149757 +.00000000 +00000-0 +10570-2 0 00001
2 40970 64.7514 181.7969 0033556 23.5222 336.7446 15.54947642 08
| Epoch (UTC): | 25 May 2026 13:42:57 |
| Eccentricity: | 0.0033556 |
| inclination: | 64.7514° |
| perigee height: | 380 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 181.7969° |
| argument of perigee: | 23.5222° |
| revolutions per day: | 15.54947642 |
| mean anomaly at epoch: | 336.7446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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