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 00082U 61004B 23150.48430522 .00000167 00000-0 16580-3 0 9997
2 00082 38.8574 170.6878 1166229 241.3457 106.5126 12.26209702940002
| Epoch (UTC): | 30 May 2023 11:37:23 |
| Eccentricity: | 0.1166229 |
| inclination: | 38.8574° |
| perigee height: | 639 km |
| apogee height: | 2492 km |
| right ascension of ascending node: | 170.6878° |
| argument of perigee: | 241.3457° |
| revolutions per day: | 12.26209702 |
| mean anomaly at epoch: | 106.5126° |
| orbit number at epoch: | 94000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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