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 26384U 00033A 23273.98254642 .00001313 00000-0 23708-3 0 9997
2 26384 97.7645 277.7031 0012494 286.1398 73.8432 14.67971445243506
| Epoch (UTC): | 30 September 2023 23:34:52 |
| Eccentricity: | 0.0012494 |
| inclination: | 97.7645° |
| perigee height: | 659 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 277.7031° |
| argument of perigee: | 286.1398° |
| revolutions per day: | 14.67971445 |
| mean anomaly at epoch: | 73.8432° |
| orbit number at epoch: | 24350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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