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 27612U 02058H 23341.26169323 .00001190 00000-0 16944-3 0 9996
2 27612 64.5555 299.4154 0019520 182.5647 177.5362 14.81433514130700
| Epoch (UTC): | 07 December 2023 06:16:50 |
| Eccentricity: | 0.0019520 |
| inclination: | 64.5555° |
| perigee height: | 611 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 299.4154° |
| argument of perigee: | 182.5647° |
| revolutions per day: | 14.81433514 |
| mean anomaly at epoch: | 177.5362° |
| orbit number at epoch: | 13070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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