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 26075.21906024 +.00000000 +00000-0 +81839-4 0 00001
2 25338 98.5156 98.3297 0009105 258.5129 101.5029 14.27115395 08
| Epoch (UTC): | 16 March 2026 05:15:26 |
| Eccentricity: | 0.0009105 |
| inclination: | 98.5156° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 98.3297° |
| argument of perigee: | 258.5129° |
| revolutions per day: | 14.27115395 |
| mean anomaly at epoch: | 101.5029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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