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 57146U 26145.44424220 +.00000000 +00000-0 +23887-4 0 00008
2 57146 43.0031 189.7261 0001849 278.0596 82.0046 15.27577421 00
| Epoch (UTC): | 25 May 2026 10:39:42 |
| Eccentricity: | 0.0001849 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.7261° |
| argument of perigee: | 278.0596° |
| revolutions per day: | 15.27577421 |
| mean anomaly at epoch: | 82.0046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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