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 40971U 26145.56287932 +.00000000 +00000-0 +27956-3 0 00006
2 40971 64.7768 345.5816 0131150 67.5027 293.9908 14.90446227 00
| Epoch (UTC): | 25 May 2026 13:30:32 |
| Eccentricity: | 0.0131150 |
| inclination: | 64.7768° |
| perigee height: | 505 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 345.5816° |
| argument of perigee: | 67.5027° |
| revolutions per day: | 14.90446227 |
| mean anomaly at epoch: | 293.9908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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