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 40012U 26110.37178574 +.00000000 +00000-0 +21604-3 0 00008
2 40012 97.7806 264.1387 0043991 258.5705 101.0568 14.87897544 03
| Epoch (UTC): | 20 April 2026 08:55:22 |
| Eccentricity: | 0.0043991 |
| inclination: | 97.7806° |
| perigee height: | 574 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 264.1387° |
| argument of perigee: | 258.5705° |
| revolutions per day: | 14.87897544 |
| mean anomaly at epoch: | 101.0568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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