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 26038.27016615 +.00000000 +00000-0 +93341-4 0 00005
2 25338 98.5187 62.3436 0010428 14.8380 345.3105 14.27099844 03
| Epoch (UTC): | 07 February 2026 06:29:02 |
| Eccentricity: | 0.0010428 |
| inclination: | 98.5187° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 62.3436° |
| argument of perigee: | 14.8380° |
| revolutions per day: | 14.27099844 |
| mean anomaly at epoch: | 345.3105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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