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 39026U 12072A 23088.73254024 .00081704 00000-0 12162-2 0 9994
2 39026 97.2840 84.0321 0019563 193.7241 166.3484 15.54632136572902
| Epoch (UTC): | 29 March 2023 17:34:51 |
| Eccentricity: | 0.0019563 |
| inclination: | 97.2840° |
| perigee height: | 390 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 84.0321° |
| argument of perigee: | 193.7241° |
| revolutions per day: | 15.54632136 |
| mean anomaly at epoch: | 166.3484° |
| orbit number at epoch: | 57290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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