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 23088.21393183 -.00000111 00000-0 -26247-3 0 9993
2 00053 47.2801 9.5328 0097758 200.4046 159.2822 12.17292923792174
| Epoch (UTC): | 29 March 2023 05:08:03 |
| Eccentricity: | 0.0097758 |
| inclination: | 47.2801° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 9.5328° |
| argument of perigee: | 200.4046° |
| revolutions per day: | 12.17292923 |
| mean anomaly at epoch: | 159.2822° |
| orbit number at epoch: | 79217 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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