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 26042.27681573 +.00000000 +00000-0 +34755-3 0 00008
2 48274 41.4684 8.7316 0004347 58.3290 301.7972 15.59483141 04
| Epoch (UTC): | 11 February 2026 06:38:36 |
| Eccentricity: | 0.0004347 |
| inclination: | 41.4684° |
| perigee height: | 386 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 8.7316° |
| argument of perigee: | 58.3290° |
| revolutions per day: | 15.59483141 |
| mean anomaly at epoch: | 301.7972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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