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 26157.09777052 +.00000000 +00000-0 +34274-3 0 00009
2 48274 41.4693 29.4663 0009357 351.5849 8.4832 15.60328974 03
| Epoch (UTC): | 06 June 2026 02:20:47 |
| Eccentricity: | 0.0009357 |
| inclination: | 41.4693° |
| perigee height: | 380 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 29.4663° |
| argument of perigee: | 351.5849° |
| revolutions per day: | 15.60328974 |
| mean anomaly at epoch: | 8.4832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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