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 29U 60002B 23337.55597459 .00001876 00000-0 29985-3 0 9994
2 29 48.3773 99.3644 0024074 245.1274 114.7135 14.75782844405227
| Epoch (UTC): | 03 December 2023 13:20:36 |
| Eccentricity: | 0.0024074 |
| inclination: | 48.3773° |
| perigee height: | 626 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 99.3644° |
| argument of perigee: | 245.1274° |
| revolutions per day: | 14.75782844 |
| mean anomaly at epoch: | 114.7135° |
| orbit number at epoch: | 40522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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