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 20465U 90010A 24279.52987851 .00015833 00000-0 11038-2 0 9991
2 20465 82.4904 197.0782 0011272 295.5420 64.4641 15.05259724884926
| Epoch (UTC): | 05 October 2024 12:43:01 |
| Eccentricity: | 0.0011272 |
| inclination: | 82.4904° |
| perigee height: | 543 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 197.0782° |
| argument of perigee: | 295.5420° |
| revolutions per day: | 15.05259724 |
| mean anomaly at epoch: | 64.4641° |
| orbit number at epoch: | 88492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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