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 48444U 26145.48116042 +.00000000 +00000-0 -87612-4 0 00000
2 48444 53.1598 181.0187 0001417 87.8317 272.2847 15.31715811 05
| Epoch (UTC): | 25 May 2026 11:32:52 |
| Eccentricity: | 0.0001417 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.0187° |
| argument of perigee: | 87.8317° |
| revolutions per day: | 15.31715811 |
| mean anomaly at epoch: | 272.2847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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