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 26088.11954713 +.00000000 +00000-0 +94660-4 0 00008
2 25338 98.5139 110.8918 0009533 216.7423 143.3106 14.27120352 06
| Epoch (UTC): | 29 March 2026 02:52:08 |
| Eccentricity: | 0.0009533 |
| inclination: | 98.5139° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 110.8918° |
| argument of perigee: | 216.7423° |
| revolutions per day: | 14.27120352 |
| mean anomaly at epoch: | 143.3106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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