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 26041.25463160 +.00000000 +00000-0 +10239-3 0 00000
2 00045 66.6951 335.9328 0255807 252.3743 104.9275 14.35866574 07
| Epoch (UTC): | 10 February 2026 06:06:40 |
| Eccentricity: | 0.0255807 |
| inclination: | 66.6951° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 335.9328° |
| argument of perigee: | 252.3743° |
| revolutions per day: | 14.35866574 |
| mean anomaly at epoch: | 104.9275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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