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 26135.21575441 +.00000000 +00000-0 +30546-4 0 00000
2 00045 66.6927 87.4071 0249199 184.9673 174.8954 14.35946956 06
| Epoch (UTC): | 15 May 2026 05:10:41 |
| Eccentricity: | 0.0249199 |
| inclination: | 66.6927° |
| perigee height: | 594 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 87.4071° |
| argument of perigee: | 184.9673° |
| revolutions per day: | 14.35946956 |
| mean anomaly at epoch: | 174.8954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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