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 38341U 12025E 24284.30565216 .00008741 00000-0 89180-3 0 9996
2 38341 98.4171 203.1510 0048717 192.5247 167.4762 14.90024621671321
| Epoch (UTC): | 10 October 2024 07:20:08 |
| Eccentricity: | 0.0048717 |
| inclination: | 98.4171° |
| perigee height: | 564 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 203.1510° |
| argument of perigee: | 192.5247° |
| revolutions per day: | 14.90024621 |
| mean anomaly at epoch: | 167.4762° |
| orbit number at epoch: | 67132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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