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 57336U 26145.38717218 +.00000000 +00000-0 +13958-4 0 00002
2 57336 43.0005 176.0574 0001072 275.8268 84.2461 15.27575794 03
| Epoch (UTC): | 25 May 2026 09:17:31 |
| Eccentricity: | 0.0001072 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 176.0574° |
| argument of perigee: | 275.8268° |
| revolutions per day: | 15.27575794 |
| mean anomaly at epoch: | 84.2461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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