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 20253U 26031.80222419 +.00000000 +00000-0 +00000-0 0 00005
2 20253 12.4586 351.9820 0008800 321.7109 231.7581 1.00279344 04
| Epoch (UTC): | 31 January 2026 19:15:12 |
| Eccentricity: | 0.0008800 |
| inclination: | 12.4586° |
| perigee height: | 35747 km |
| apogee height: | 35822 km |
| right ascension of ascending node: | 351.9820° |
| argument of perigee: | 321.7109° |
| revolutions per day: | 1.00279344 |
| mean anomaly at epoch: | 231.7581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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