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 26548U 26038.73605720 +.00000000 +00000-0 +34305-3 0 00005
2 26548 64.5473 177.9178 0034707 305.1301 54.6562 15.00923173 09
| Epoch (UTC): | 07 February 2026 17:39:55 |
| Eccentricity: | 0.0034707 |
| inclination: | 64.5473° |
| perigee height: | 540 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 177.9178° |
| argument of perigee: | 305.1301° |
| revolutions per day: | 15.00923173 |
| mean anomaly at epoch: | 54.6562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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