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 57371U 26145.53936109 +.00000000 +00000-0 +61259-4 0 00007
2 57371 43.0025 167.5668 0001375 270.9177 89.1517 15.26738548 07
| Epoch (UTC): | 25 May 2026 12:56:40 |
| Eccentricity: | 0.0001375 |
| inclination: | 43.0025° |
| perigee height: | 485 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 167.5668° |
| argument of perigee: | 270.9177° |
| revolutions per day: | 15.26738548 |
| mean anomaly at epoch: | 89.1517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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