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 48453U 26145.38327516 +.00000000 +00000-0 +25185-4 0 00005
2 48453 53.1598 181.3976 0001150 92.0300 268.0833 15.31707906 02
| Epoch (UTC): | 25 May 2026 09:11:54 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.3976° |
| argument of perigee: | 92.0300° |
| revolutions per day: | 15.31707906 |
| mean anomaly at epoch: | 268.0833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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