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 40032U 14033Y 23158.40564884 .00003778 00000-0 36878-3 0 9998
2 40032 97.9680 98.8369 0009985 334.2433 25.8287 14.93006440486513
| Epoch (UTC): | 07 June 2023 09:44:08 |
| Eccentricity: | 0.0009985 |
| inclination: | 97.9680° |
| perigee height: | 581 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 98.8369° |
| argument of perigee: | 334.2433° |
| revolutions per day: | 14.93006440 |
| mean anomaly at epoch: | 25.8287° |
| orbit number at epoch: | 48651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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