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 26134.58889713 +.00000000 +00000-0 +33162-4 0 00006
2 00045 66.6926 89.0651 0249256 185.4244 174.4151 14.35946853 02
| Epoch (UTC): | 14 May 2026 14:08:00 |
| Eccentricity: | 0.0249256 |
| inclination: | 66.6926° |
| perigee height: | 594 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 89.0651° |
| argument of perigee: | 185.4244° |
| revolutions per day: | 14.35946853 |
| mean anomaly at epoch: | 174.4151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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