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 25143.83368611 .00000655 00000-0 11878-3 0 9994
2 29 48.3787 73.8934 0022279 31.0005 329.2218 14.77978907484636
| Epoch (UTC): | 23 May 2025 20:00:30 |
| Eccentricity: | 0.0022279 |
| inclination: | 48.3787° |
| perigee height: | 620 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 73.8934° |
| argument of perigee: | 31.0005° |
| revolutions per day: | 14.77978907 |
| mean anomaly at epoch: | 329.2218° |
| orbit number at epoch: | 48463 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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