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 57608U 26145.33623742 +.00000000 +00000-0 +41274-4 0 00009
2 57608 43.0060 9.1274 0001168 273.9533 86.1185 15.27577636 00
| Epoch (UTC): | 25 May 2026 08:04:10 |
| Eccentricity: | 0.0001168 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 9.1274° |
| argument of perigee: | 273.9533° |
| revolutions per day: | 15.27577636 |
| mean anomaly at epoch: | 86.1185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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