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 26545U 26032.29970970 +.00000000 +00000-0 +21935-3 0 00004
2 26545 64.5536 4.4721 0032715 319.9205 39.9492 14.92716747 02
| Epoch (UTC): | 01 February 2026 07:11:34 |
| Eccentricity: | 0.0032715 |
| inclination: | 64.5536° |
| perigee height: | 567 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 4.4721° |
| argument of perigee: | 319.9205° |
| revolutions per day: | 14.92716747 |
| mean anomaly at epoch: | 39.9492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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