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 39134U 13015E 23088.80624831 .00094989 00000-0 17888-2 0 9996
2 39134 64.8537 196.5662 0019025 258.4574 101.4431 15.47801218550643
| Epoch (UTC): | 29 March 2023 19:20:59 |
| Eccentricity: | 0.0019025 |
| inclination: | 64.8537° |
| perigee height: | 410 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 196.5662° |
| argument of perigee: | 258.4574° |
| revolutions per day: | 15.47801218 |
| mean anomaly at epoch: | 101.4431° |
| orbit number at epoch: | 55064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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