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 23082.89627607 .00001657 00000-0 29961-3 0 9998
2 26384 97.7661 96.4789 0014308 168.3651 191.7888 14.67545465214703
| Epoch (UTC): | 23 March 2023 21:30:38 |
| Eccentricity: | 0.0014308 |
| inclination: | 97.7661° |
| perigee height: | 659 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 96.4789° |
| argument of perigee: | 168.3651° |
| revolutions per day: | 14.67545465 |
| mean anomaly at epoch: | 191.7888° |
| orbit number at epoch: | 21470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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