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 40974U 26145.53753164 +.00000000 +00000-0 +49664-3 0 00001
2 40974 64.7598 246.8415 0078296 56.7100 304.1492 15.15674654 03
| Epoch (UTC): | 25 May 2026 12:54:02 |
| Eccentricity: | 0.0078296 |
| inclination: | 64.7598° |
| perigee height: | 465 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 246.8415° |
| argument of perigee: | 56.7100° |
| revolutions per day: | 15.15674654 |
| mean anomaly at epoch: | 304.1492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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