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 39136U 13015G 23332.58946708 .00172789 00000-0 17460-2 0 9996
2 39136 64.8564 152.0819 0018842 256.6965 103.2083 15.64318701587143
| Epoch (UTC): | 28 November 2023 14:08:49 |
| Eccentricity: | 0.0018842 |
| inclination: | 64.8564° |
| perigee height: | 362 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 152.0819° |
| argument of perigee: | 256.6965° |
| revolutions per day: | 15.64318701 |
| mean anomaly at epoch: | 103.2083° |
| orbit number at epoch: | 58714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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