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 48580U 26145.34557250 +.00000000 +00000-0 +45102-4 0 00003
2 48580 53.1593 104.4815 0001265 90.6254 269.4893 15.31701587 05
| Epoch (UTC): | 25 May 2026 08:17:37 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.4815° |
| argument of perigee: | 90.6254° |
| revolutions per day: | 15.31701587 |
| mean anomaly at epoch: | 269.4893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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