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 37391U 11014B 23157.05251794 0.00000000 00000-0 00000-0 0 04
2 37391 63.4340 225.8086 0260582 357.2187 2.7813 13.40883368 07
| Epoch (UTC): | 06 June 2023 01:15:37 |
| Eccentricity: | 0.0260582 |
| inclination: | 63.4340° |
| perigee height: | 911 km |
| apogee height: | 1301 km |
| right ascension of ascending node: | 225.8086° |
| argument of perigee: | 357.2187° |
| revolutions per day: | 13.40883368 |
| mean anomaly at epoch: | 2.7813° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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