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 40296U 26103.37621176 +.00000000 +00000-0 +00000-0 0 00009
2 40296 63.4495 221.7366 6672014 270.9872 19.2720 2.00583615 03
| Epoch (UTC): | 13 April 2026 09:01:44 |
| Eccentricity: | 0.6672014 |
| inclination: | 63.4495° |
| perigee height: | 2461 km |
| apogee height: | 37900 km |
| right ascension of ascending node: | 221.7366° |
| argument of perigee: | 270.9872° |
| revolutions per day: | 2.00583615 |
| mean anomaly at epoch: | 19.2720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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