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 26162.21782795 +.00000000 +00000-0 +24653-3 0 00009
2 48274 41.4694 358.3237 0008197 28.9315 331.1976 15.60563857 05
| Epoch (UTC): | 11 June 2026 05:13:40 |
| Eccentricity: | 0.0008197 |
| inclination: | 41.4694° |
| perigee height: | 380 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 358.3237° |
| argument of perigee: | 28.9315° |
| revolutions per day: | 15.60563857 |
| mean anomaly at epoch: | 331.1976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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