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 26109.29307865 +.00000000 +00000-0 +50944-4 0 00008
2 25338 98.5114 131.5060 0010783 154.2596 205.9124 14.27127993 06
| Epoch (UTC): | 19 April 2026 07:02:01 |
| Eccentricity: | 0.0010783 |
| inclination: | 98.5114° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 131.5060° |
| argument of perigee: | 154.2596° |
| revolutions per day: | 14.27127993 |
| mean anomaly at epoch: | 205.9124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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