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 22220U 92076B 25191.61039470 .00000185 00000-0 11609-3 0 9994
2 22220 71.0011 338.2898 0010781 106.9057 338.4576 14.16808567687548
| Epoch (UTC): | 10 July 2025 14:38:58 |
| Eccentricity: | 0.0010781 |
| inclination: | 71.0011° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 338.2898° |
| argument of perigee: | 106.9057° |
| revolutions per day: | 14.16808567 |
| mean anomaly at epoch: | 338.4576° |
| orbit number at epoch: | 68754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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