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 57668U 26145.44396745 +.00000000 +00000-0 +25721-4 0 00006
2 57668 53.1596 210.5242 0001224 84.6048 275.5093 15.30191608 03
| Epoch (UTC): | 25 May 2026 10:39:18 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.5242° |
| argument of perigee: | 84.6048° |
| revolutions per day: | 15.30191608 |
| mean anomaly at epoch: | 275.5093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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