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 13068U 82013B 23147.16781208 .00001675 00000-0 99674-4 0 9990
2 13068 81.1835 262.0232 0030404 344.0164 16.0099 15.10331086250466
| Epoch (UTC): | 27 May 2023 04:01:38 |
| Eccentricity: | 0.0030404 |
| inclination: | 81.1835° |
| perigee height: | 514 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 262.0232° |
| argument of perigee: | 344.0164° |
| revolutions per day: | 15.10331086 |
| mean anomaly at epoch: | 16.0099° |
| orbit number at epoch: | 25046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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