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 24286.81128927 0.00013500 00000-0 10865-2 0 00
2 23605 98.2771 127.1630 0009613 302.3176 57.6823 14.99989661 06
| Epoch (UTC): | 12 October 2024 19:28:15 |
| Eccentricity: | 0.0009613 |
| inclination: | 98.2771° |
| perigee height: | 560 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 127.1630° |
| argument of perigee: | 302.3176° |
| revolutions per day: | 14.99989661 |
| mean anomaly at epoch: | 57.6823° |
| 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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