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 00045U 26047.17524207 +.00000000 +00000-0 +89810-4 0 00009
2 00045 66.6947 320.2745 0255561 248.1673 109.2069 14.35871514 03
| Epoch (UTC): | 16 February 2026 04:12:20 |
| Eccentricity: | 0.0255561 |
| inclination: | 66.6947° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 320.2745° |
| argument of perigee: | 248.1673° |
| revolutions per day: | 14.35871514 |
| mean anomaly at epoch: | 109.2069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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