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 40012U 14033C 23155.52368855 .00002508 00000-0 35548-3 0 9999
2 40012 97.6717 330.2017 0057124 97.3981 263.3726 14.76736203481908
| Epoch (UTC): | 04 June 2023 12:34:06 |
| Eccentricity: | 0.0057124 |
| inclination: | 97.6717° |
| perigee height: | 599 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 330.2017° |
| argument of perigee: | 97.3981° |
| revolutions per day: | 14.76736203 |
| mean anomaly at epoch: | 263.3726° |
| orbit number at epoch: | 48190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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