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 26039.60229566 +.00000000 +00000-0 +82917-4 0 00001
2 25338 98.5187 63.6411 0010348 11.0074 349.1331 14.27100317 01
| Epoch (UTC): | 08 February 2026 14:27:18 |
| Eccentricity: | 0.0010348 |
| inclination: | 98.5187° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 63.6411° |
| argument of perigee: | 11.0074° |
| revolutions per day: | 14.27100317 |
| mean anomaly at epoch: | 349.1331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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