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 57955U 26145.37862117 +.00000000 +00000-0 +37984-4 0 00002
2 57955 53.1622 17.9965 0001341 88.0746 272.0408 15.30191819 02
| Epoch (UTC): | 25 May 2026 09:05:12 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.1622° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 17.9965° |
| argument of perigee: | 88.0746° |
| revolutions per day: | 15.30191819 |
| mean anomaly at epoch: | 272.0408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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