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 02680U 67014A 23082.94072009 .00002160 00000-0 89524-3 0 9990
2 02680 39.4398 306.4574 0713279 156.0344 207.5362 13.39259188717431
| Epoch (UTC): | 23 March 2023 22:34:38 |
| Eccentricity: | 0.0713279 |
| inclination: | 39.4398° |
| perigee height: | 578 km |
| apogee height: | 1646 km |
| right ascension of ascending node: | 306.4574° |
| argument of perigee: | 156.0344° |
| revolutions per day: | 13.39259188 |
| mean anomaly at epoch: | 207.5362° |
| orbit number at epoch: | 71743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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