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 data is extracted from the following two-line orbital elements,
1 40129U 14050B 25082.00275700 .00000004 00000-0 00000-0 0 9998
2 40129 49.3820 290.8954 1623168 162.7355 203.5175 1.85520469 72111
| Epoch (UTC): | 23 March 2025 00:03:58 |
| Eccentricity: | 0.1623168 |
| inclination: | 49.3820° |
| perigee height: | 17058 km |
| apogee height: | 26140 km |
| right ascension of ascending node: | 290.8954° |
| argument of perigee: | 162.7355° |
| revolutions per day: | 1.85520469 |
| mean anomaly at epoch: | 203.5175° |
| orbit number at epoch: | 7211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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