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 20041U 26150.40632550 +.00000000 +00000-0 +00000-0 0 00009
2 20041 13.9986 346.6922 0013526 313.0240 259.3544 1.00650310 05
| Epoch (UTC): | 30 May 2026 09:45:06 |
| Eccentricity: | 0.0013526 |
| inclination: | 13.9986° |
| perigee height: | 35624 km |
| apogee height: | 35738 km |
| right ascension of ascending node: | 346.6922° |
| argument of perigee: | 313.0240° |
| revolutions per day: | 1.00650310 |
| mean anomaly at epoch: | 259.3544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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