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 26848U 26088.00308503 +.00000000 +00000-0 +46618-4 0 00003
2 26848 81.2740 292.0238 0011275 187.4603 172.6402 14.10115305 06
| Epoch (UTC): | 29 March 2026 00:04:26 |
| Eccentricity: | 0.0011275 |
| inclination: | 81.2740° |
| perigee height: | 851 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 292.0238° |
| argument of perigee: | 187.4603° |
| revolutions per day: | 14.10115305 |
| mean anomaly at epoch: | 172.6402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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