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 55378U 26145.29849367 +.00000000 +00000-0 +46139-4 0 00004
2 55378 43.0013 248.5297 0001363 263.6602 96.4094 15.27580465 01
| Epoch (UTC): | 25 May 2026 07:09:49 |
| Eccentricity: | 0.0001363 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 248.5297° |
| argument of perigee: | 263.6602° |
| revolutions per day: | 15.27580465 |
| mean anomaly at epoch: | 96.4094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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