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 20453U 90008B 24283.80375418 .00036740 00000-0 12152-2 0 9999
2 20453 35.6164 209.0194 0187551 302.7474 55.5298 15.15120000846883
| Epoch (UTC): | 09 October 2024 19:17:24 |
| Eccentricity: | 0.0187551 |
| inclination: | 35.6164° |
| perigee height: | 391 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 209.0194° |
| argument of perigee: | 302.7474° |
| revolutions per day: | 15.15120000 |
| mean anomaly at epoch: | 55.5298° |
| orbit number at epoch: | 84688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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