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 40964U 15058A 26011.18706910 0.00000000 00000-0 00000-0 0 07
2 40964 63.4420 114.0481 0199586 358.5481 1.4519 13.40993200 06
| Epoch (UTC): | 11 January 2026 04:29:22 |
| Eccentricity: | 0.0199586 |
| inclination: | 63.4420° |
| perigee height: | 956 km |
| apogee height: | 1255 km |
| right ascension of ascending node: | 114.0481° |
| argument of perigee: | 358.5481° |
| revolutions per day: | 13.40993200 |
| mean anomaly at epoch: | 1.4519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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