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 22025.13958004 -.00000018 00000-0 28175-4 0 9997
2 29 48.3803 59.5947 0024489 223.7688 136.1283 14.74510542305231
| Epoch (UTC): | 25 January 2022 03:20:59 |
| Eccentricity: | 0.0024489 |
| inclination: | 48.3803° |
| perigee height: | 629 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 59.5947° |
| argument of perigee: | 223.7688° |
| revolutions per day: | 14.74510542 |
| mean anomaly at epoch: | 136.1283° |
| orbit number at epoch: | 30523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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