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 26142.59560066 +.00000000 +00000-0 +55469-4 0 00009
2 25338 98.5078 163.9185 0011371 65.8280 294.4088 14.27137805 08
| Epoch (UTC): | 22 May 2026 14:17:39 |
| Eccentricity: | 0.0011371 |
| inclination: | 98.5078° |
| perigee height: | 793 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 163.9185° |
| argument of perigee: | 65.8280° |
| revolutions per day: | 14.27137805 |
| mean anomaly at epoch: | 294.4088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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