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 27607U 02058C 23083.60762662 .00004585 00000-0 63803-3 0 9993
2 27607 64.5556 164.1816 0075740 241.4775 117.8688 14.77001493 89737
| Epoch (UTC): | 24 March 2023 14:34:58 |
| Eccentricity: | 0.0075740 |
| inclination: | 64.5556° |
| perigee height: | 585 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 164.1816° |
| argument of perigee: | 241.4775° |
| revolutions per day: | 14.77001493 |
| mean anomaly at epoch: | 117.8688° |
| orbit number at epoch: | 8973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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