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 26069.48347081 +.00000000 +00000-0 +33669-3 0 00006
2 48274 41.4662 203.3317 0006956 277.6291 82.3758 15.60703934 00
| Epoch (UTC): | 10 March 2026 11:36:11 |
| Eccentricity: | 0.0006956 |
| inclination: | 41.4662° |
| perigee height: | 381 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 203.3317° |
| argument of perigee: | 277.6291° |
| revolutions per day: | 15.60703934 |
| mean anomaly at epoch: | 82.3758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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