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 48441U 26145.36465075 +.00000000 +00000-0 +45211-4 0 00005
2 48441 53.1582 181.5958 0001238 57.9055 302.2066 15.31701124 03
| Epoch (UTC): | 25 May 2026 08:45:05 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.5958° |
| argument of perigee: | 57.9055° |
| revolutions per day: | 15.31701124 |
| mean anomaly at epoch: | 302.2066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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