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 57262U 26145.46053804 +.00000000 +00000-0 +10618-3 0 00002
2 57262 43.0028 306.0995 0001537 278.4725 81.5952 15.27572568 02
| Epoch (UTC): | 25 May 2026 11:03:10 |
| Eccentricity: | 0.0001537 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.0995° |
| argument of perigee: | 278.4725° |
| revolutions per day: | 15.27572568 |
| mean anomaly at epoch: | 81.5952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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