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 26086.42573529 +.00000000 +00000-0 +00000-0 0 00003
2 40296 63.4571 223.4310 6678556 271.0900 19.1383 2.00582684 06
| Epoch (UTC): | 27 March 2026 10:13:03 |
| Eccentricity: | 0.6678556 |
| inclination: | 63.4571° |
| perigee height: | 2443 km |
| apogee height: | 37918 km |
| right ascension of ascending node: | 223.4310° |
| argument of perigee: | 271.0900° |
| revolutions per day: | 2.00582684 |
| mean anomaly at epoch: | 19.1383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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