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 06155U 72065B 25348.61953765 .00001494 00000-0 20799-3 0 9999
2 06155 35.0016 84.1854 0033714 13.4464 346.7129 14.77416111828670
| Epoch (UTC): | 14 December 2025 14:52:08 |
| Eccentricity: | 0.0033714 |
| inclination: | 35.0016° |
| perigee height: | 614 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 84.1854° |
| argument of perigee: | 13.4464° |
| revolutions per day: | 14.77416111 |
| mean anomaly at epoch: | 346.7129° |
| orbit number at epoch: | 82867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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