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 48469U 26145.37705308 +.00000000 +00000-0 +30348-4 0 00007
2 48469 53.1587 194.4976 0001334 90.6778 269.4376 15.31697566 06
| Epoch (UTC): | 25 May 2026 09:02:57 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.4976° |
| argument of perigee: | 90.6778° |
| revolutions per day: | 15.31697566 |
| mean anomaly at epoch: | 269.4376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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