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 26546U 26038.57644616 +.00000000 +00000-0 +36270-3 0 00005
2 26546 64.5504 124.1825 0036527 297.6062 62.1347 15.04575959 00
| Epoch (UTC): | 07 February 2026 13:50:04 |
| Eccentricity: | 0.0036527 |
| inclination: | 64.5504° |
| perigee height: | 527 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 124.1825° |
| argument of perigee: | 297.6062° |
| revolutions per day: | 15.04575959 |
| mean anomaly at epoch: | 62.1347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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