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 57368U 26145.48676877 +.00000000 +00000-0 -37087-4 0 00003
2 57368 43.0019 168.0308 0001034 278.6826 81.3909 15.27579463 00
| Epoch (UTC): | 25 May 2026 11:40:56 |
| Eccentricity: | 0.0001034 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.0308° |
| argument of perigee: | 278.6826° |
| revolutions per day: | 15.27579463 |
| mean anomaly at epoch: | 81.3909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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