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 26104.22102389 +.00000000 +00000-0 +61864-4 0 00001
2 00045 66.6928 169.3900 0252083 207.3881 151.3747 14.35933322 08
| Epoch (UTC): | 14 April 2026 05:18:16 |
| Eccentricity: | 0.0252083 |
| inclination: | 66.6928° |
| perigee height: | 592 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 169.3900° |
| argument of perigee: | 207.3881° |
| revolutions per day: | 14.35933322 |
| mean anomaly at epoch: | 151.3747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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