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 08344U 75094B 24280.64305687 .00001671 00000-0 53678-3 0 9996
2 08344 74.0547 246.9760 0022199 202.9835 157.0329 14.40045430569309
| Epoch (UTC): | 06 October 2024 15:26:00 |
| Eccentricity: | 0.0022199 |
| inclination: | 74.0547° |
| perigee height: | 742 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 246.9760° |
| argument of perigee: | 202.9835° |
| revolutions per day: | 14.40045430 |
| mean anomaly at epoch: | 157.0329° |
| orbit number at epoch: | 56930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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