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 23089.77537251 .00106875 00000-0 19953-2 0 9995
2 39134 64.8536 193.2897 0018862 259.2362 100.6656 15.48001469550795
| Epoch (UTC): | 30 March 2023 18:36:32 |
| Eccentricity: | 0.0018862 |
| inclination: | 64.8536° |
| perigee height: | 410 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 193.2897° |
| argument of perigee: | 259.2362° |
| revolutions per day: | 15.48001469 |
| mean anomaly at epoch: | 100.6656° |
| orbit number at epoch: | 55079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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