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 00694U 63047A 23031.26402602 .00001779 00000-0 21510-3 0 9996
2 00694 30.3606 12.8177 0579124 229.8209 125.0285 14.04279502971728
| Epoch (UTC): | 31 January 2023 06:20:11 |
| Eccentricity: | 0.0579124 |
| inclination: | 30.3606° |
| perigee height: | 459 km |
| apogee height: | 1299 km |
| right ascension of ascending node: | 12.8177° |
| argument of perigee: | 229.8209° |
| revolutions per day: | 14.04279502 |
| mean anomaly at epoch: | 125.0285° |
| orbit number at epoch: | 97172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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