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 23085.90970029 .00002516 00000-0 35934-3 0 9992
2 27607 64.5550 157.1273 0075571 241.0454 118.3058 14.77014157 90079
| Epoch (UTC): | 26 March 2023 21:49:58 |
| Eccentricity: | 0.0075571 |
| inclination: | 64.5550° |
| perigee height: | 586 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 157.1273° |
| argument of perigee: | 241.0454° |
| revolutions per day: | 14.77014157 |
| mean anomaly at epoch: | 118.3058° |
| orbit number at epoch: | 9007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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