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 47748U 26145.66668980 +.00000000 +00000-0 +78981-2 0 00005
2 47748 53.1527 180.7082 0001143 67.7337 181.1725 15.75230415 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1527° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 180.7082° |
| argument of perigee: | 67.7337° |
| revolutions per day: | 15.75230415 |
| mean anomaly at epoch: | 181.1725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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