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 57067U 26145.40306851 +.00000000 +00000-0 -42295-6 0 00002
2 57067 43.0047 37.5015 0001115 268.1733 91.8991 15.27577310 09
| Epoch (UTC): | 25 May 2026 09:40:25 |
| Eccentricity: | 0.0001115 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.5015° |
| argument of perigee: | 268.1733° |
| revolutions per day: | 15.27577310 |
| mean anomaly at epoch: | 91.8991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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