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 00053U 60009E 24280.86683637 .00000026 00000-0 10973-2 0 9996
2 00053 47.2754 89.6008 0099803 49.1199 311.8185 12.17350451860103
| Epoch (UTC): | 06 October 2024 20:48:14 |
| Eccentricity: | 0.0099803 |
| inclination: | 47.2754° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 89.6008° |
| argument of perigee: | 49.1199° |
| revolutions per day: | 12.17350451 |
| mean anomaly at epoch: | 311.8185° |
| orbit number at epoch: | 86010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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