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 40981U 15058R 26011.18715421 0.00000000 00000-0 00000-0 0 03
2 40981 63.4486 114.2994 0198832 358.0270 1.9730 13.40993843 05
| Epoch (UTC): | 11 January 2026 04:29:30 |
| Eccentricity: | 0.0198832 |
| inclination: | 63.4486° |
| perigee height: | 957 km |
| apogee height: | 1254 km |
| right ascension of ascending node: | 114.2994° |
| argument of perigee: | 358.0270° |
| revolutions per day: | 13.40993843 |
| mean anomaly at epoch: | 1.9730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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