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 48274U 26108.04590214 +.00000000 +00000-0 +22357-3 0 00002
2 48274 41.4679 328.3459 0006178 229.5609 130.4692 15.62499605 09
| Epoch (UTC): | 18 April 2026 01:06:05 |
| Eccentricity: | 0.0006178 |
| inclination: | 41.4679° |
| perigee height: | 376 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 328.3459° |
| argument of perigee: | 229.5609° |
| revolutions per day: | 15.62499605 |
| mean anomaly at epoch: | 130.4692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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