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 57245U 26145.50038322 +.00000000 +00000-0 -76703-4 0 00005
2 57245 43.0044 306.4036 0001503 278.1551 81.9131 15.27553786 02
| Epoch (UTC): | 25 May 2026 12:00:33 |
| Eccentricity: | 0.0001503 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.4036° |
| argument of perigee: | 278.1551° |
| revolutions per day: | 15.27553786 |
| mean anomaly at epoch: | 81.9131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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