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 57638U 26145.34892248 +.00000000 +00000-0 -57756-4 0 00005
2 57638 43.0058 8.2603 0001084 262.2153 97.8576 15.27563364 08
| Epoch (UTC): | 25 May 2026 08:22:26 |
| Eccentricity: | 0.0001084 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.2603° |
| argument of perigee: | 262.2153° |
| revolutions per day: | 15.27563364 |
| mean anomaly at epoch: | 97.8576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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