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 37380U 10062M 23081.51830507 .00001970 00000-0 26556-3 0 9997
2 37380 71.9707 257.3968 0016614 181.8808 178.2296 14.80246035190509
| Epoch (UTC): | 22 March 2023 12:26:21 |
| Eccentricity: | 0.0016614 |
| inclination: | 71.9707° |
| perigee height: | 617 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 257.3968° |
| argument of perigee: | 181.8808° |
| revolutions per day: | 14.80246035 |
| mean anomaly at epoch: | 178.2296° |
| orbit number at epoch: | 19050 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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