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 15945U 85069B 24252.51115408 .00002030 00000-0 23233-3 0 9993
2 15945 82.5303 179.1265 0018463 199.6177 160.4331 14.85419733112670
| Epoch (UTC): | 08 September 2024 12:16:03 |
| Eccentricity: | 0.0018463 |
| inclination: | 82.5303° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 179.1265° |
| argument of perigee: | 199.6177° |
| revolutions per day: | 14.85419733 |
| mean anomaly at epoch: | 160.4331° |
| orbit number at epoch: | 11267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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