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 26046.18307446 +.00000000 +00000-0 +27285-3 0 00006
2 48274 41.4683 345.0034 0004127 100.2382 259.8922 15.59646494 02
| Epoch (UTC): | 15 February 2026 04:23:37 |
| Eccentricity: | 0.0004127 |
| inclination: | 41.4683° |
| perigee height: | 386 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 345.0034° |
| argument of perigee: | 100.2382° |
| revolutions per day: | 15.59646494 |
| mean anomaly at epoch: | 259.8922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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