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 26067.81967659 +.00000000 +00000-0 +34617-3 0 00004
2 48274 41.4664 213.4556 0006999 268.3248 91.6789 15.60610742 06
| Epoch (UTC): | 08 March 2026 19:40:20 |
| Eccentricity: | 0.0006999 |
| inclination: | 41.4664° |
| perigee height: | 381 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 213.4556° |
| argument of perigee: | 268.3248° |
| revolutions per day: | 15.60610742 |
| mean anomaly at epoch: | 91.6789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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