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 48571U 26145.38339961 +.00000000 +00000-0 +22947-4 0 00006
2 48571 53.1593 142.8440 0001226 90.7471 269.3671 15.31702027 07
| Epoch (UTC): | 25 May 2026 09:12:05 |
| Eccentricity: | 0.0001226 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 142.8440° |
| argument of perigee: | 90.7471° |
| revolutions per day: | 15.31702027 |
| mean anomaly at epoch: | 269.3671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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