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 04857U 70025EM 24280.76599920 .00011745 00000-0 50338-2 0 9990
2 04857 99.7822 103.6619 0047818 48.7954 311.7329 14.24365127735314
| Epoch (UTC): | 06 October 2024 18:23:02 |
| Eccentricity: | 0.0047818 |
| inclination: | 99.7822° |
| perigee height: | 776 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 103.6619° |
| argument of perigee: | 48.7954° |
| revolutions per day: | 14.24365127 |
| mean anomaly at epoch: | 311.7329° |
| orbit number at epoch: | 73531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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