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 24256.38146451 .00002308 00000-0 19526-2 0 9990
2 00082 38.8537 226.2352 1165371 355.6194 3.4985 12.27007689997821
| Epoch (UTC): | 12 September 2024 09:09:18 |
| Eccentricity: | 0.1165371 |
| inclination: | 38.8537° |
| perigee height: | 637 km |
| apogee height: | 2487 km |
| right ascension of ascending node: | 226.2352° |
| argument of perigee: | 355.6194° |
| revolutions per day: | 12.27007689 |
| mean anomaly at epoch: | 3.4985° |
| orbit number at epoch: | 99782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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