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 27610U 02058F 23032.51054076 .00000067 00000-0 50933-4 0 9996
2 27610 64.5587 69.7135 0281105 30.1470 71.7977 14.28352985 48913
| Epoch (UTC): | 01 February 2023 12:15:10 |
| Eccentricity: | 0.0281105 |
| inclination: | 64.5587° |
| perigee height: | 595 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 69.7135° |
| argument of perigee: | 30.1470° |
| revolutions per day: | 14.28352985 |
| mean anomaly at epoch: | 71.7977° |
| orbit number at epoch: | 4891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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