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 48572U 26145.39931014 +.00000000 +00000-0 -95090-5 0 00006
2 48572 53.1619 152.1353 0001392 99.3497 260.7661 15.31699198 09
| Epoch (UTC): | 25 May 2026 09:35:00 |
| Eccentricity: | 0.0001392 |
| inclination: | 53.1619° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 152.1353° |
| argument of perigee: | 99.3497° |
| revolutions per day: | 15.31699198 |
| mean anomaly at epoch: | 260.7661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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