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 47879U 26145.37941575 +.00000000 +00000-0 +12601-2 0 00009
2 47879 53.1549 276.0698 0002601 263.6208 96.4506 15.50304574 02
| Epoch (UTC): | 25 May 2026 09:06:21 |
| Eccentricity: | 0.0002601 |
| inclination: | 53.1549° |
| perigee height: | 414 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 276.0698° |
| argument of perigee: | 263.6208° |
| revolutions per day: | 15.50304574 |
| mean anomaly at epoch: | 96.4506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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