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 23078.78505952 .00073671 00000-0 14864-2 0 9990
2 39134 64.8537 230.3908 0020284 251.8434 108.0497 15.45878170549095
| Epoch (UTC): | 19 March 2023 18:50:29 |
| Eccentricity: | 0.0020284 |
| inclination: | 64.8537° |
| perigee height: | 415 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 230.3908° |
| argument of perigee: | 251.8434° |
| revolutions per day: | 15.45878170 |
| mean anomaly at epoch: | 108.0497° |
| orbit number at epoch: | 54909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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