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 23080.42399051 .00000373 00000-0 33817-3 0 9995
2 00082 38.8621 70.0688 1167373 263.1408 83.5377 12.26140257931401
| Epoch (UTC): | 21 March 2023 10:10:32 |
| Eccentricity: | 0.1167373 |
| inclination: | 38.8621° |
| perigee height: | 638 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 70.0688° |
| argument of perigee: | 263.1408° |
| revolutions per day: | 12.26140257 |
| mean anomaly at epoch: | 83.5377° |
| orbit number at epoch: | 93140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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