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 26159.08188282 +.00000000 +00000-0 +30374-3 0 00008
2 48274 41.4696 17.3987 0008703 5.5904 354.5031 15.60427341 07
| Epoch (UTC): | 08 June 2026 01:57:54 |
| Eccentricity: | 0.0008703 |
| inclination: | 41.4696° |
| perigee height: | 381 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 17.3987° |
| argument of perigee: | 5.5904° |
| revolutions per day: | 15.60427341 |
| mean anomaly at epoch: | 354.5031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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