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 26066.60376234 +.00000000 +00000-0 +30832-3 0 00008
2 48274 41.4662 220.8523 0006959 260.1334 99.8719 15.60534588 08
| Epoch (UTC): | 07 March 2026 14:29:25 |
| Eccentricity: | 0.0006959 |
| inclination: | 41.4662° |
| perigee height: | 381 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 220.8523° |
| argument of perigee: | 260.1334° |
| revolutions per day: | 15.60534588 |
| mean anomaly at epoch: | 99.8719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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