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 39136U 13015G 22026.78476797 .00004757 00000-0 22784-3 0 9998
2 39136 64.8744 205.7652 0011082 262.9408 97.0459 15.20116680484849
| Epoch (UTC): | 26 January 2022 18:50:03 |
| Eccentricity: | 0.0011082 |
| inclination: | 64.8744° |
| perigee height: | 498 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 205.7652° |
| argument of perigee: | 262.9408° |
| revolutions per day: | 15.20116680 |
| mean anomaly at epoch: | 97.0459° |
| orbit number at epoch: | 48484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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