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 57928U 26145.03607728 +.00000000 +00000-0 +11949-4 0 00003
2 57928 43.0023 257.4956 0001081 301.0503 59.0243 15.27575799 05
| Epoch (UTC): | 25 May 2026 00:51:57 |
| Eccentricity: | 0.0001081 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 257.4956° |
| argument of perigee: | 301.0503° |
| revolutions per day: | 15.27575799 |
| mean anomaly at epoch: | 59.0243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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