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 40908U 15049K 24277.19561744 .00023171 00000-0 80507-3 0 9996
2 40908 97.5235 286.9189 0010351 340.7778 19.3070 15.29703644499983
| Epoch (UTC): | 03 October 2024 04:41:41 |
| Eccentricity: | 0.0010351 |
| inclination: | 97.5235° |
| perigee height: | 469 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 286.9189° |
| argument of perigee: | 340.7778° |
| revolutions per day: | 15.29703644 |
| mean anomaly at epoch: | 19.3070° |
| orbit number at epoch: | 49998 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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