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 23083.50634558 .00147175 00000-0 28454-2 0 9992
2 39134 64.8544 214.4670 0019570 255.2025 104.6948 15.46813552550204
| Epoch (UTC): | 24 March 2023 12:09:08 |
| Eccentricity: | 0.0019570 |
| inclination: | 64.8544° |
| perigee height: | 413 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 214.4670° |
| argument of perigee: | 255.2025° |
| revolutions per day: | 15.46813552 |
| mean anomaly at epoch: | 104.6948° |
| orbit number at epoch: | 55020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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