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 23085.70426278 .00089167 00000-0 17141-2 0 9991
2 39134 64.8539 207.0466 0019401 256.4004 103.4975 15.47226088550167
| Epoch (UTC): | 26 March 2023 16:54:08 |
| Eccentricity: | 0.0019401 |
| inclination: | 64.8539° |
| perigee height: | 411 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 207.0466° |
| argument of perigee: | 256.4004° |
| revolutions per day: | 15.47226088 |
| mean anomaly at epoch: | 103.4975° |
| orbit number at epoch: | 55016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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