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 25338U 26285.33818794 +.00000000 +00000-0 +65786-4 0 00006
2 25338 98.5033 302.7899 0010381 10.7212 349.4189 14.27174834 04
| Epoch (UTC): | 12 October 2026 08:06:59 |
| Eccentricity: | 0.0010381 |
| inclination: | 98.5033° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 302.7899° |
| argument of perigee: | 10.7212° |
| revolutions per day: | 14.27174834 |
| mean anomaly at epoch: | 349.4189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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