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 40013U 26071.24182000 +.00000000 +00000-0 +44857-4 0 00006
2 40013 97.5971 309.0749 0000880 51.6864 308.4435 14.93417308 03
| Epoch (UTC): | 12 March 2026 05:48:13 |
| Eccentricity: | 0.0000880 |
| inclination: | 97.5971° |
| perigee height: | 587 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 309.0749° |
| argument of perigee: | 51.6864° |
| revolutions per day: | 14.93417308 |
| mean anomaly at epoch: | 308.4435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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