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 23605U 95033A 24277.80498408 0.00011000 00000-0 89062-3 0 02
2 23605 98.2811 117.5438 0009613 332.1394 27.8604 14.99760343 03
| Epoch (UTC): | 03 October 2024 19:19:10 |
| Eccentricity: | 0.0009613 |
| inclination: | 98.2811° |
| perigee height: | 561 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 117.5438° |
| argument of perigee: | 332.1394° |
| revolutions per day: | 14.99760343 |
| mean anomaly at epoch: | 27.8604° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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