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 26017.75917748 +.00000000 +00000-0 +23896-3 0 00003
2 48274 41.4657 157.7848 0011174 305.0077 54.9713 15.60612084 02
| Epoch (UTC): | 17 January 2026 18:13:12 |
| Eccentricity: | 0.0011174 |
| inclination: | 41.4657° |
| perigee height: | 378 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 157.7848° |
| argument of perigee: | 305.0077° |
| revolutions per day: | 15.60612084 |
| mean anomaly at epoch: | 54.9713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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