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 29048U 06011B 25190.74965026 .00000261 00000-0 11399-3 0 9992
2 29048 71.9642 201.9689 0040565 71.7494 288.8051 14.30971227 7781
| Epoch (UTC): | 09 July 2025 17:59:29 |
| Eccentricity: | 0.0040565 |
| inclination: | 71.9642° |
| perigee height: | 759 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 201.9689° |
| argument of perigee: | 71.7494° |
| revolutions per day: | 14.30971227 |
| mean anomaly at epoch: | 288.8051° |
| orbit number at epoch: | 778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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