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 48576U 26145.19179020 +.00000000 +00000-0 +25899-3 0 00006
2 48576 53.1574 105.2507 0001393 75.5433 284.5723 15.31701645 04
| Epoch (UTC): | 25 May 2026 04:36:10 |
| Eccentricity: | 0.0001393 |
| inclination: | 53.1574° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 105.2507° |
| argument of perigee: | 75.5433° |
| revolutions per day: | 15.31701645 |
| mean anomaly at epoch: | 284.5723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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