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 57090U 26145.38686672 +.00000000 +00000-0 +25025-4 0 00006
2 57090 43.0065 22.6773 0001638 258.5347 101.5321 15.27580534 03
| Epoch (UTC): | 25 May 2026 09:17:05 |
| Eccentricity: | 0.0001638 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 22.6773° |
| argument of perigee: | 258.5347° |
| revolutions per day: | 15.27580534 |
| mean anomaly at epoch: | 101.5321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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