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 26549U 26039.18767060 +.00000000 +00000-0 +22915-3 0 00006
2 26549 64.5499 39.4462 0031402 328.8524 31.0724 14.90777753 02
| Epoch (UTC): | 08 February 2026 04:30:14 |
| Eccentricity: | 0.0031402 |
| inclination: | 64.5499° |
| perigee height: | 574 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 39.4462° |
| argument of perigee: | 328.8524° |
| revolutions per day: | 14.90777753 |
| mean anomaly at epoch: | 31.0724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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