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 57470U 26145.66668980 +.00000000 +00000-0 +25341-2 0 00000
2 57470 43.0002 269.6255 0001303 274.9390 65.4740 15.28127813 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001303 |
| inclination: | 43.0002° |
| perigee height: | 481 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 269.6255° |
| argument of perigee: | 274.9390° |
| revolutions per day: | 15.28127813 |
| mean anomaly at epoch: | 65.4740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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