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 28654U 05018A 24262.80183445 .00000506 00000-0 29311-3 0 9998
2 28654 98.8685 338.9691 0014799 154.7077 205.4823 14.13332485996485
| Epoch (UTC): | 18 September 2024 19:14:38 |
| Eccentricity: | 0.0014799 |
| inclination: | 98.8685° |
| perigee height: | 837 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 338.9691° |
| argument of perigee: | 154.7077° |
| revolutions per day: | 14.13332485 |
| mean anomaly at epoch: | 205.4823° |
| orbit number at epoch: | 99648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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