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 is defined by the following mean orbital elements,
1 20625U 26159.18244838 +.00000000 +00000-0 +18107-3 0 00009
2 20625 70.9982 107.8591 0014077 175.3297 184.7960 14.15021434 06
| Epoch (UTC): | 08 June 2026 04:22:43 |
| Eccentricity: | 0.0014077 |
| inclination: | 70.9982° |
| perigee height: | 832 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 107.8591° |
| argument of perigee: | 175.3297° |
| revolutions per day: | 14.15021434 |
| mean anomaly at epoch: | 184.7960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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